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929:) fueled thrusters. Eight of those were to provide altitude control and the remaining eight for controlling the orbital velocity. The VTM stage also provided pitch, yaw and roll control during the orbital insertion maneuvers. The three main stages of the SSLV-D1 functioned normally. But, that was not enough to impart adequate impulse for the two satellite payloads to achieve stable orbits. For the injection of the two satellite payloads into their intended stable orbits, the VTM stage had to fire for at least 20 seconds, to impart enough additional orbital velocity and altitude corrections. Instead the VTM kicked-in at 653.5s and shut itself down at 653.6s, post lift-off. Following the partial firing of the VTM stage, the EOS 02 was released at 738.5s and AazadiSAT at 788.4s, post-liftoff. These failures transpired, resulting in the satellites entering an unstable orbit and subsequently destroyed upon reentry.
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1002:. After seventeen minutes, the EOS-08 was injected into a 475 km circular orbit, following the instructed injection conditions without any deviations. The SSLV development process is now officially complete. The development team will continue to search for specific operational activities in the VTM stage before ISRO supplies the industry with SSLV technology for serial production. Any necessary fine-tuning will be finished prior to the technology transfer. With a 72-hour turnaround time, the ability to support several satellites, a small launch infrastructure requirement with a team of 6 people, and the possibility of launch on demand, SSLV is now a cost-effective solution. Repeatable flight performance of the SSLV vehicle systems has also been demonstrated by SSLV-D3. The successful flight of SSLV-D3 permits the Indian private sector and
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2745:"SSLV-D1/EOS-02 Mission update: SSLV-D1 placed the satellites into 356 km x 76 km elliptical orbit instead of 356 km circular orbit. Satellites are no longer usable. Issue is reasonably identified. Failure of a logic to identify a sensor failure and go for a salvage action caused the deviation. A committee would analyse and recommend. With the implementation of the recommendations, ISRO will come back soon with SSLV-D2. A detailed statement by Chairman, ISRO will be uploaded soon"
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performance runs show that SSLV-1 is capable of putting a 350 kg satellite in a polar orbit of 511 km x 497 km orbit and a 400 kg satellite in an orbit of 425 x 401 km (higher payloads are possible in equatorial orbit). This payload capability allows the launch of microsatellites with optical imaging and radar imaging payloads as well as individual intelligence satellites. Satellite life for the 400 kg mass satellite may be short in the 400 km orbit.
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detected vibrations that were longer in duration and more intense during the second stage of separation. In order to ensure that this problem doesn't occur again, the second stage detachment system in SSLV-D2 was modified to reduce vibrations. Furthermore, the system was redesigned to navigate utilizing
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The SSLV Project was completed after more than seven years of construction. Six companies are now in the process of acquiring the SSLV technology, while at least ten companies and consortia have expressed interest in manufacturing. The integration and launch time of SSLV rocket is less than 24 hours.
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The separation mechanism, the equipment bay, and the on-board system for identifying malfunctioning sensors were further modified and five new pieces of hardware were installed. The electronics in SSLV-D2 worked successfully, as did the launch vehicle's new, affordable guidance and navigation system.
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After analyzing the problems with SSLV-D1, ISRO chose the necessary remedial measures and put them into practice. The development team conducted a number of simulations and studies to make sure that SSLV-D2 mission would succeed. According to SSLV-D1 fault evaluation study, six onboard accelerometers
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satellites into their orbits about 1.6 minutes later. The purpose of SSLV-D2 is to launch the three satellites into a 450-kilometer circular orbit and showcase the in-flight performance of the SSLV vehicle systems. A total of 175.2 kilograms was carried by the SSLV-D2: 10.2 kg for Janus-1, 8.7 kg for
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During the open loop guidance mode, the final VTM stage only managed to fire for 0.1s instead of the intended 20s. This led to the two satellites as well as the VTM stage of the rocket being injected into an unstable elliptical transatmospheric orbit of 360.56×75.66 km with an inclination of 36.56°.
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The development of SSLV is in the final stages and the first developmental flight of SSLV is targeted during the first quarter of 2022. The
Government has sanctioned a total cost of Rs.169.07 Crores for the development project including the development & qualification of the vehicle systems and
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The projected high launch rate relies on largely autonomous launch operation and on overall simple logistics. To compare, a PSLV launch involves 600 officials while SSLV launch operations would be managed by a small team of about six people. The launch readiness period of the SSLV is expected to be
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The official explanation by the ISRO for the mission failure was software malfunction. According to the ISRO, the mission software detected an accelerometer anomaly during the second stage separation. This caused the rocket navigation to switch from a closed loop guidance to an open loop guidance.
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The first static fire test (ST01) of the SS1 first-stage booster conducted on 18 March 2021 was unsuccessful. About 60 seconds into the test, oscillations were observed and after 95 seconds, the nozzle of SS1 stage disintegrated. The nominal duration of test was 110 seconds. To qualify for flight,
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By appropriate choice from among the solid propellant stages available with ISRO and DRDO, a launch vehicle could be configured and designated Small
Satellite Launch Vehicle (SSLV-1). The performance of SSLV-1 was estimated using the in house developed trajectory-modelling programme QuoVadis. The
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The first static test of SS1 solid motor was conducted and the performance of SS1 ignition system, propellant system and Flex Nozzle
Control (FNC) system was evaluated. Various design modifications have been incorporated to resolve the anomalies observed in the first static test
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1434:"The launch of the SSLV-D1/EOS-02 Mission is scheduled for Sunday, August 7, 2022, at 9:18 am (IST) from Satish Dhawan Space Centre (SDSC), Sriharikota. ISRO invites citizens to the Launch View Gallery at SDSC to witness the launch"
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based solid propellant, with a fourth terminal stage being a
Velocity-Trimming Module (VTM) with eight 50 N thrusters for reaction control and eight 50 N axial thrusters for changing velocity. With these VTM can add
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SSLV is made keeping low cost, low turnaround time in mind with launch-on-demand flexibility under minimal infrastructure requirements. It is capable of carrying multiple satellites. Once SSLV is operational,
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This
Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
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According to a former ISRO scientist, the VTM can correct for a velocity shortfall of up to 172 metres/s. The rocket used for SSLV-D1 was a 34 m tall, 2 m diameter vehicle having a lift-off mass of 120
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also acknowledged a need for identifying a cost effective launch vehicle configuration with 500 kg payload capacity to LEO and by
November 2017, development of such launch vehicle was underway.
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The rocket had a three stage configuration with a fourth
Velocity Trimming Module (VTM). In its D1 configuration, the rocket was 34m tall with a diameter of 2m and a lift-off mass of 120t.
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2719:"SSLV-D1/EOS-02 Mission: Maiden flight of SSLV is completed. All stages performed as expected. Data loss is observed during the terminal stage. It is being analysed. Will be updated soon"
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It may be specifically noted that process toolings of composite motor case for 2nd stage of SSLV is interchangeable with composite motor case for 3rd stage of PSLV to maximum extent.
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report by
Rajaram Nagappa proposed development path of a 'Small Satellite launch Vehicle-1' to launch strategic payloads. In National Space Science Symposium 2016, then Director of
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The proposed systems will be used as a part of new commanding requirement for Small
Satellite Launch Vehicle (SSLV) Launch Complex (SLC) Site at Kulasekarapatnam, Tamilnadu.
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on 7 August 2022, however, the payload failed to reach the intended orbit. The second flight SSLV-D2 was successful in delivering payload into orbit on 10 February 2023.
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On 10 February 2023, SSLV completed its second developmental mission, putting three satellites into their planned orbits. The three-stage rocket successfully launched
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In
December 2020, all booster segments for SSLV first stage (SS1) static test (ST01) were received and assembly was done in Second Vehicle Assembly Building (SVAB).
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Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
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1710:"Spaceflight Inc. Purchases and Fully Manifests First-Ever Commercial SSLV Mission from NewSpace India Limited (NSIL), the Commercial Arm of ISRO, India"
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793:. Tenders related to manufacturing, installation, assembly, inspection, testing and Self Propelled launching Unit (SPU) were released in October 2019.
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Two solid stages are new, fully developed. That is SS1 with 85-90 tonnes and SS3 with 4.5 tonnes whereas SS2 is almost identical to the HPS3 of PSLV.
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The SSLV was developed with the aim of launching small satellites commercially at drastically reduced price and higher launch rate compared to
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education. The SSLV-D1 was supposed to place the two satellite payloads in a circular orbit of altitude 356.2 km with 37.2° inclination.
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Even though, this switch in guidance mode was part of the redundancy built into the rocket's navigation, it could not salvage the mission.
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The first stage (SS1) and third stage (SS3) of SSLV are newly developed while second stage (SS2) is derived from third stage (HPS3) of
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The second static fire test of SSLV first stage SS1 was conducted on 14 March 2022 at SDSC-SHAR and met the required test objectives.
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less than a week instead of months. The launch vehicle can be assembled both vertically like the existing PSLV and
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This article is about the small-lift rocket developed by ISRO in the 2020s. For similarly named 1970s rocket, see
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699:(US$ 4.2 million). According to analysts, this places it among the most affordable rockets in its class.
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2796:"ISRO chief S. Somanath interview | 'An anomaly for two seconds led to SSLV mission's underperformance'"
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1684:"SSLV-D1/EOS-02 mission: Rocket injected satellites but orbit achieved is less than expected, Isro says"
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2989:"ISRO successfully launches SSLV's second developmental flight with three satellites from Sriharikota"
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2123:"Design, Fabrication, Integration, Testing, Supply and Commissioning of Vehicle Telecommand Systems"
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190 crore or US$ 23 million in 2023) and the manufacturing cost is expected to be
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2855:"India's new small satellite launcher fails to put satellites into correct orbit – Spaceflight Now"
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REQUEST FOR PROPOSAL (RFP) FOR PROCUREMENT, MANUFACTURE, SUPPLY, TESTING and COMMISIONING [
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REQUEST FOR PROPOSAL (RFP) FOR SUPPLY, INSTALLATION AND COMMISSIONING OF RAIL TRACK FOR SLC PROJECT
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906:, a CubeSat payload that weighed 8 kg, developed by Indian students to promote inclusivity in
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The first developmental flight of the SSLV occurred on 7 August 2022. The flight mission was named
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SSLV-D1/EOS-02 Mission launch is scheduled for Aug 7, 2022 at 9:18 hrs IST from SDSC, Sriharikota
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SSLV-D1/EOS-02 Mission launch is scheduled for Aug 7, 2022 at 9:18 hrs IST from SDSC, Sriharikota
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1802:"Isro successfully launches SSLV-D3: Why is this mission significant for India's space sector?"
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2415:"Future of Space Transportation by S. Somanath (Director, Liquid Propulsion Systems Centre)"
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The SSLV Payload Fairing (SPLF) functional qualification test was completed in August 2021.
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the flight demonstration through three development flights (SSLV-D1, SSLV-D2 & SSLV-D3)
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3134:"Isro's SSLV-D3 mission successful, EOS-08 and SR-0 Demosat satellites placed in orbit"
2628:"Ground testing of Solid Booster Stage (SS1) for Small Satellite Launch Vehicle (SSLV)"
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data and readings will now be monitored for a longer time before entering rescue mode.
2829:"ISRO's Maiden Small Satellite Rocket Flight Ends in Doubt After Engine Fails to Fire"
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2071:"Episode 90 – An update on ISRO's activities with S. Somanath and R. Umamaheshwaran"
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Dr. Somnath on ISRO's Roadmap and Indian Launch Vehicles at Toulouse Space Show 2018
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3167:"Isro SSLV-D3 mission: Why it could forever change India's satellite launch market"
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1828:"India's 19 upcoming missions, and ISRO's Small Satellite Launch Vehicle (SSLV)"
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1408:"'We have a new launch vehicle': Isro successfully introduces SSLV to the world"
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1326:"Why ISRO's maiden SSLV mission failed despite successful launch of new rocket"
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2440:"Isro news: A rocket that can be made in 3 days | India News - Times of India"
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The early developmental flights and those to inclined orbits will launch from
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1772:"There's big money to make in space business for Indian firms: Antrix chief"
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into a circular orbit around 13 minutes after liftoff. Also, Janus-1 and
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2305:"ISRO's Second Spaceport, for New SSLV Rocket, to Come up in Tamil Nadu"
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3220:"Explained: Why is ISRO's third developmental flight SSLV-D3 unique?"
2607:"Monthly Summary of Department of space for the month of August 2021"
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2099:. Indian Space Research Organisation. 1 January 2019. Archived from
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SSLV's solid first stage SS1 has to perform two consecutive nominal
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Indian National Space Promotion and Authorisation Centre (IN–SPACe)
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892:. The SSLV-D1 flight failed to achieve its mission objectives.
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1655:"Successful flight of Small Satellite Launch Vehicle (SSLV)"
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34:. For small-lift satellite launch vehicles in general, see
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1983:. 15 August 2022. Event occurs at 2 minutes 40 seconds.
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Indian Institute of Space Science and Technology (IIST)
3023:"Mission accomplished: ISRO's SSLV-D2 launch explained"
2361:"The Promise of Small Satellites for National Security"
2189:"TENDER NOTICE NO. SDSC SHAR/Sr.HPS/PT/RO/03/2019-2020"
1746:"ISRO to rope in industry majors for mini-PSLV project"
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500 kg in 500 km orbit at 35° to 55° inclination range.
621:(NSIL) and a group of Indian companies will manage the
1932:. 6 August 2022. Event occurs at 2 minute 30 seconds.
1633:"ISRO plans to launch new rocket before December 2020"
1276:"ISRO readying for low cost satellite launch vehicles"
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Single/Multi Satellites - Nano, Micro, Mini satellites
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10 kg (22 lb) to 500 kg (1,100 lb)
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Development and Educational Communication Unit (DECU)
1576:"Department of Space presentation on 18 January 2019"
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Indian Space Research Organisation (1 August 2022).
2232:"TENDER NOTICE NO. SDSC SHAR/Sr.HPS/PT/11/2019-2020"
2150:"TENDER NOTICE NO. SDSC SHAR/Sr.HPS/PT/13/2019-2020"
1850:"ISRO developing vehicle to launch small satellites"
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1300:"Chandrayaan-2 Mission planned for middle of April"
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590:to deliver 500 kg (1,100 lb) payload to
2466:"Design for Small Satellite Launch Vehicle ready"
1872:"Design for Small Satellite Launch Vehicle ready"
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3049:"SSLV-D2 places three small satellites in orbit"
2258:RFP document for Supply of Stainless Steel Tanks
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921:The SSLV-D1's final VTM stage had 16 hydrazine (
602:supports multi-orbital drop-offs capability for
5245:National Atmospheric Research Laboratory (NARL)
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884:and Velocity Trimming Module (VTM) upper stage.
5861:Development and Educational Communication Unit
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844:(VSSC) completed the design for the vehicle.
609:The maiden flight SSLV-D1 was conducted from
512:Fourth stage – Velocity Trimming Module (VTM)
5887:ISRO Telemetry, Tracking and Command Network
2551:"Department of Space, Annual Report 2021-22"
2525:"చిన్న ఉపగ్రహ వాహకనౌక మోటారులో సాంకేతికలోపం"
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1508:
1506:
1504:
1502:
1500:
1498:
1465:
1463:
1461:
1459:
1006:to use the rocket for operational flights.
6014:List of Satish Dhawan Space Centre launches
2793:
2759:
2063:
1370:
1368:
1366:
1364:
57:Satish Dhawan Space Centre First Launch Pad
5793:Thumba Equatorial Rocket Launching Station
5182:
5168:
3289:
3282:
3268:
2571:
1289:
1265:
718:The first three stages of the vehicle use
151:120 t (120 long tons; 130 short tons)
49:
5240:Indian Institute of Remote Sensing (IIRS)
5225:Indian Space Research Organisation (ISRO)
1495:
1456:
1013:
707:(GSLV) and horizontally like the retired
2987:Kandavel, Sangeetha (10 February 2023).
2986:
2955:"ISRO launches SSLV-D2 from Sriharikota"
2821:
1707:
1361:
981:
936:
873:
659:(PSLV). The development cost of SSLV is
632:
2358:
1194:Geosynchronous Satellite Launch Vehicle
962:AzaadiSAT-2, and 156.3 kg for EOS-07.
705:Geosynchronous Satellite Launch Vehicle
14:
6037:
5687:RLV Technology Demonstration Programme
864:
827:National Institute of Advanced Studies
774:
628:
5851:Laboratory for Electro-Optics Systems
5163:
3263:
3217:
3020:
2463:
2269:
2219:] OF SELF PROPELLED UNITS FOR SLC
1796:
1794:
1743:
1739:
1737:
1599:
1388:from the original on 20 December 2019
3307:Comparison of orbital launch systems
3106:
3046:
2794:Subramanian, T. s (11 August 2022).
2373:from the original on 14 January 2017
2046:"Indian Space Research Organisation"
1929:SSLV-D1/EOS-02 Mission Video_English
1769:
1246:
1244:
1084:Decade-wise summary of SSLV launches
1024:
3072:
3021:Singh, Abhinav (10 February 2023).
2612:. 29 September 2021. Archived from
2438:Surendra Singh (22 November 2017).
2270:Singh, Surendra (2 December 2019).
2128:. 16 September 2020. Archived from
1897:Ramachandran, R. (26 August 2022).
1890:
1647:
1630:
24:
5561:Indian human spaceflight programme
5255:Physical Research Laboratory (PRL)
2741:Indian Space Research Organization
2733:
2715:Indian Space Research Organization
2707:
2620:
2359:Nagappa, Rajaram (December 2015).
2319:
2115:
1980:SHAR Director Rajarajan Press Meet
1949:. 19 February 2020. Archived from
1791:
1734:
1701:
1681:
1543:
1184:Indian Space Research Organisation
713:Augmented Satellite Launch Vehicle
25:
6071:
3241:
3218:Singh, Abhinav (13 August 2024).
3047:Dutt, Anonna (10 February 2023).
2852:
2420:. 7 February 2016. Archived from
2399:. 7 February 2016. Archived from
1241:
598:(500 km (310 mi)). The
122:(US$ 4.2 million) (expected)
5882:Indian Space Science Data Centre
5831:Liquid Propulsion Systems Centre
5283:
5191:
3247:
2501:. 1 January 2021. Archived from
2464:Rajwi, Tiki (21 December 2018).
1830:. SpaceTech Asia. 28 August 2018
1708:Sorensen, Jodi (6 August 2019).
1682:U., Tejonmayam (7 August 2022).
1518:"Small Satellite Launch Vehicle"
1471:"SSLV-D1/EOS-2 Mission Brochure"
1163:
1149:
1135:
990:The Earth Observation Satellite
831:Liquid Propulsion Systems Centre
357:87,000 kg (192,000 lb)
27:Indian small-lift launch vehicle
6055:Expendable space launch systems
5527:Lunar Polar Exploration Mission
5135:Super heavy-lift launch vehicle
3211:
3185:
3159:
3126:
3107:Dutt, Anonna (16 August 2024).
3100:
3073:C.S, Hemanth (16 August 2024).
3066:
3040:
3014:
2980:
2947:
2914:
2891:
2868:
2846:
2787:
2685:"SSLV-D1/EOS-02 Mission - ISRO"
2677:
2652:
2636:. 14 March 2022. Archived from
2599:
2556:. 27 April 2022. Archived from
2543:
2517:
2491:
2457:
2431:
2407:
2389:
2352:
2327:""Industrialised" PSLV by 2022"
2297:
2263:
2224:
2181:
2142:
2085:
2038:
2015:
1990:
1936:
1864:
1842:
1820:
1763:
1675:
1600:Kumar, Chethan (19 July 2022).
1531:
1410:. India Today. 10 February 2023
536:16 × 50N bipropellant thrusters
6045:Small Satellite Launch Vehicle
5897:National Remote Sensing Centre
3302:List of orbital launch systems
3254:Small Satellite Launch Vehicle
2093:"Message from Chairman's desk"
2073:. AstrotalkUK. 24 October 2019
2022:Narayan Prasad (4 July 2018),
1744:Singh, Surendra (4 May 2018).
1400:
1340:
1318:
1216:
1204:Next Generation Launch Vehicle
1189:Polar Satellite Launch Vehicle
986:EOS-08 prior to encapsulation.
820:
657:Polar Satellite Launch Vehicle
576:Small Satellite Launch Vehicle
414:7,700 kg (17,000 lb)
143:2 m (6 ft 7 in)
44:Small Satellite Launch Vehicle
13:
1:
5250:NewSpace India Limited (NSIL)
1376:"SSLV technical brochure V12"
1328:. Dnaindia.com. 8 August 2022
1209:
808:will handle SSLV launches to
471:4,500 kg (9,900 lb)
5821:Vikram Sarabhai Space Centre
842:Vikram Sarabhai Space Centre
798:Kulasekarapattinam Spaceport
285:Kulasekarapattinam Spaceport
7:
6060:Vehicles introduced in 2022
5803:Kulasekharapatnam Spaceport
5357:Human Spaceflight Programme
1128:
781:Kulasekharapatnam Spaceport
10:
6076:
6050:ISRO space launch vehicles
5846:ISRO Inertial Systems Unit
5788:Satish Dhawan Space Centre
5281:
5125:Medium-lift launch vehicle
1252:"Satellite Launch Vehicle"
1017:
996:Satish Dhawan Space Centre
977:
932:
869:
815:
800:, under development, near
778:
687:(US$ 3.6 million) to
282:Satish Dhawan Space Centre
110:(US$ 3.6 million) to
29:
6024:List of ISRO chairpersons
6009:List of Indian satellites
6004:
5972:
5921:
5905:
5877:Indian Deep Space Network
5869:
5856:Human Space Flight Centre
5841:Space Applications Centre
5813:
5778:
5758:
5732:
5725:
5700:
5679:
5612:
5603:
5553:
5453:
5421:
5365:
5292:
5217:
5209:Department of Space (DoS)
5204:
5143:
5130:Heavy-lift launch vehicle
5120:Small-lift launch vehicle
5107:
3957:
3731:
3315:
3297:
1770:IANS (2 September 2018).
1179:Small-lift launch vehicle
766:Up to 300 kg into 500 km
584:small-lift launch vehicle
561:
557:
540:
532:
524:
516:
511:
499:
491:
483:
475:
467:
459:
454:
442:
434:
426:
418:
410:
402:
397:
385:
377:
369:
361:
353:
345:
340:
336:
328:
316:
308:
300:
290:
277:
269:
264:
233:
228:
224:
220:300 kg (660 lb)
216:
212:500 km (310 mi)
208:
200:
192:
184:
180:500 km (310 mi)
176:
168:
163:
155:
147:
139:
131:
126:
95:
87:
73:
68:Small-lift launch vehicle
63:
55:SSLV D1 lifting off from
48:
36:Small-lift launch vehicle
5826:U R Rao Satellite Centre
1660:Press Information Bureau
709:Satellite Launch Vehicle
528:50 kg (110 lb)
32:Satellite Launch Vehicle
5892:Master Control Facility
5836:ISRO Propulsion Complex
1777:Business Standard India
1631:Service, Tribune News.
738:Vehicle characteristics
727:of up to 172 m/s.
625:and launch activities.
135:34 m (112 ft)
5906:Legislation and policy
5538:Mars Orbiter Mission 2
5198:Indian space programme
3291:Orbital launch systems
2241:. ISRO. Archived from
2159:. ISRO. Archived from
1903:frontline.thehindu.com
1014:SSLV launch statistics
1004:NewSpace India Limited
987:
950:
885:
840:By December 2018, the
652:
619:NewSpace India Limited
332:16 August 2024, EOS-08
6019:List of ISRO missions
5913:Space Activities Bill
5544:Venus Orbiter Mission
5265:Integrated Space Cell
1537:Gunter's space page:
1020:List of SSLV launches
1018:Further information:
985:
940:
877:
810:Sun-synchronous orbit
768:sun-synchronous orbit
755:Payloads capabilities
636:
596:Sun-synchronous orbit
203:Sun-synchronous orbit
5533:Mars Orbiter Mission
5456:planetary spacecraft
5408:South Asia Satellite
5270:Defence Space Agency
3256:at Wikimedia Commons
2961:. 10 February 2023.
2928:. 10 February 2023.
2616:on 29 December 2021.
1381:. 20 December 2019.
1257:. 16 December 2021.
1228:/www.nsilindia.co.in
1224:"SSLV MANUFACTURING"
5959:Bellatrix Aerospace
5814:Research facilities
5422:Space observatories
2499:"SDSC-SHAR Website"
2427:on 7 February 2016.
2403:on 7 February 2016.
2333:. 25 January 2020.
2205:on 6 September 2019
1635:. Tribuneindia News
898:The rocket carried
865:Operational history
775:SSLV Launch Complex
629:Vehicle description
185:Orbital inclination
45:
5991:Statio Shiv Shakti
5980:National Space Day
5799:under development
5594:ISRO Space Station
5230:Antrix Corporation
4297:v1.2 "Full Thrust"
3140:. 16 August 2024.
3138:The Times of India
3113:The Indian Express
3053:The Indian Express
2959:The Economic Times
2926:The Times of India
2586:The Economic Times
2563:on 27 April 2022.
2444:The Times of India
2276:The Times of India
2135:on 6 August 2022.
1878:. 21 December 2018
1750:The Times of India
1688:The Times of India
1663:. 10 February 2023
1607:The Times of India
1555:space.skyrocket.de
1171:Spaceflight portal
988:
951:
886:
747:Diameter: 2 meters
653:
398:Second stage – SS2
229:Associated rockets
43:
6032:
6031:
5934:Skyroot Aerospace
5922:Private companies
5774:
5773:
5721:
5720:
5554:Human spaceflight
5468:Moon Impact Probe
5157:
5156:
3252:Media related to
3197:Business Standard
2743:(7 August 2022).
2717:(7 August 2022).
2505:on 1 January 2021
2248:on 16 August 2019
2166:on 16 August 2019
2103:on 2 January 2019
1581:. 18 January 2019
1306:. 11 January 2019
1126:
1125:
1025:Launch statistics
853:static fire tests
802:Kulasekharapatnam
791:Kulasekharapatnam
744:Height: 34 meters
572:
571:
455:Third stage – SS3
341:First stage – SS1
88:Country of origin
16:(Redirected from
6067:
5730:
5729:
5610:
5609:
5287:
5196:
5195:
5184:
5177:
5170:
5161:
5160:
5006:Universal Rocket
3377:Falcon 9 Block 5
3284:
3277:
3270:
3261:
3260:
3251:
3235:
3234:
3232:
3230:
3215:
3209:
3208:
3206:
3204:
3199:. 20 August 2024
3189:
3183:
3182:
3180:
3178:
3163:
3157:
3156:
3154:
3152:
3130:
3124:
3123:
3121:
3119:
3104:
3098:
3097:
3095:
3093:
3070:
3064:
3063:
3061:
3059:
3044:
3038:
3037:
3035:
3033:
3018:
3012:
3011:
3009:
3007:
2984:
2978:
2977:
2975:
2973:
2951:
2945:
2944:
2942:
2940:
2918:
2912:
2911:
2910:
2908:
2895:
2889:
2888:
2887:
2885:
2872:
2866:
2865:
2863:
2861:
2853:Clark, Stephen.
2850:
2844:
2843:
2841:
2839:
2825:
2819:
2818:
2816:
2814:
2791:
2785:
2784:
2782:
2780:
2766:
2757:
2756:
2737:
2731:
2730:
2711:
2705:
2704:
2702:
2700:
2695:on 7 August 2022
2691:. Archived from
2681:
2675:
2674:
2672:
2670:
2664:Ahmedabad Mirror
2656:
2650:
2649:
2647:
2645:
2640:on 20 March 2022
2624:
2618:
2617:
2611:
2603:
2597:
2596:
2594:
2592:
2578:
2569:
2568:
2562:
2555:
2547:
2541:
2540:
2538:
2536:
2521:
2515:
2514:
2512:
2510:
2495:
2489:
2488:
2486:
2484:
2461:
2455:
2454:
2452:
2450:
2435:
2429:
2428:
2426:
2419:
2411:
2405:
2404:
2393:
2387:
2386:
2380:
2378:
2372:
2365:
2356:
2350:
2349:
2347:
2345:
2323:
2317:
2316:
2314:
2312:
2301:
2295:
2294:
2292:
2290:
2267:
2261:
2260:
2255:
2253:
2247:
2236:
2228:
2222:
2221:
2212:
2210:
2204:
2198:. Archived from
2193:
2185:
2179:
2178:
2173:
2171:
2165:
2154:
2146:
2140:
2139:
2134:
2127:
2119:
2113:
2112:
2110:
2108:
2089:
2083:
2082:
2080:
2078:
2067:
2061:
2060:
2058:
2056:
2042:
2036:
2035:
2034:
2032:
2019:
2013:
2012:
2010:
2008:
1998:"ORF on Twitter"
1994:
1988:
1987:
1975:
1969:
1968:
1963:
1961:
1955:
1948:
1940:
1934:
1933:
1924:
1918:
1917:
1911:
1909:
1894:
1888:
1887:
1885:
1883:
1868:
1862:
1861:
1859:
1857:
1846:
1840:
1839:
1837:
1835:
1824:
1818:
1817:
1815:
1813:
1808:. 16 August 2024
1798:
1789:
1788:
1786:
1784:
1767:
1761:
1760:
1758:
1756:
1741:
1732:
1731:
1729:
1727:
1722:on 6 August 2019
1718:. Archived from
1705:
1699:
1698:
1696:
1694:
1679:
1673:
1672:
1670:
1668:
1651:
1645:
1644:
1642:
1640:
1628:
1619:
1618:
1616:
1614:
1597:
1591:
1590:
1588:
1586:
1580:
1572:
1566:
1565:
1563:
1561:
1547:
1541:
1535:
1529:
1528:
1526:
1524:
1514:
1493:
1492:
1490:
1488:
1483:on 3 August 2022
1482:
1476:. Archived from
1475:
1467:
1454:
1453:
1447:
1445:
1429:
1420:
1419:
1417:
1415:
1404:
1398:
1397:
1395:
1393:
1387:
1380:
1372:
1359:
1358:
1356:
1354:
1344:
1338:
1337:
1335:
1333:
1322:
1316:
1315:
1313:
1311:
1296:
1287:
1286:
1284:
1282:
1272:
1263:
1262:
1256:
1248:
1239:
1238:
1236:
1234:
1220:
1173:
1168:
1167:
1166:
1159:
1154:
1153:
1152:
1145:
1140:
1139:
1138:
1099:Partial success
1090:
1089:
1076:
1070:
1064:
1058:
1000:first launch pad
941:Primary payload
750:Mass: 120 tonnes
698:
693:
686:
681:
674:
670:
665:
646:First Launch Pad
644:- Lift-off from
611:First Launch Pad
604:small satellites
565:edit on Wikidata
324:, 7 August 2022.
121:
116:
109:
104:
53:
46:
42:
21:
6075:
6074:
6070:
6069:
6068:
6066:
6065:
6064:
6035:
6034:
6033:
6028:
6000:
5987:(supercomputer)
5968:
5917:
5901:
5865:
5809:
5770:
5754:
5717:
5696:
5675:
5605:Launch vehicles
5599:
5549:
5455:
5449:
5417:
5393:Megha-Tropiques
5361:
5288:
5279:
5213:
5200:
5190:
5188:
5158:
5153:
5139:
5115:Sounding rocket
5103:
3953:
3727:
3311:
3293:
3288:
3244:
3239:
3238:
3228:
3226:
3216:
3212:
3202:
3200:
3191:
3190:
3186:
3176:
3174:
3173:. 8 August 2024
3165:
3164:
3160:
3150:
3148:
3132:
3131:
3127:
3117:
3115:
3105:
3101:
3091:
3089:
3071:
3067:
3057:
3055:
3045:
3041:
3031:
3029:
3019:
3015:
3005:
3003:
2985:
2981:
2971:
2969:
2953:
2952:
2948:
2938:
2936:
2920:
2919:
2915:
2906:
2904:
2903:, 6 August 2022
2897:
2896:
2892:
2883:
2881:
2880:, 6 August 2022
2874:
2873:
2869:
2859:
2857:
2851:
2847:
2837:
2835:
2827:
2826:
2822:
2812:
2810:
2792:
2788:
2778:
2776:
2774:www.isro.gov.in
2768:
2767:
2760:
2738:
2734:
2712:
2708:
2698:
2696:
2689:www.isro.gov.in
2683:
2682:
2678:
2668:
2666:
2658:
2657:
2653:
2643:
2641:
2626:
2625:
2621:
2609:
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2604:
2600:
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2413:
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2325:
2324:
2320:
2310:
2308:
2303:
2302:
2298:
2288:
2286:
2268:
2264:
2251:
2249:
2245:
2234:
2230:
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2225:
2208:
2206:
2202:
2191:
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2186:
2182:
2169:
2167:
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2152:
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2143:
2132:
2125:
2121:
2120:
2116:
2106:
2104:
2091:
2090:
2086:
2076:
2074:
2069:
2068:
2064:
2054:
2052:
2050:www.isro.gov.in
2044:
2043:
2039:
2030:
2028:
2020:
2016:
2006:
2004:
1996:
1995:
1991:
1977:
1976:
1972:
1959:
1957:
1953:
1946:
1942:
1941:
1937:
1926:
1925:
1921:
1907:
1905:
1895:
1891:
1881:
1879:
1870:
1869:
1865:
1855:
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1848:
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1826:
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1821:
1811:
1809:
1800:
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1768:
1764:
1754:
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1742:
1735:
1725:
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1706:
1702:
1692:
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1164:
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1157:Rocketry portal
1155:
1150:
1148:
1141:
1136:
1134:
1131:
1081:
1080:
1074:
1068:
1065:Partial failure
1062:
1056:
1052:
1051:
1050:
1047:
1044:
1040:
1039:
1036:
1033:
1027:
1022:
1016:
980:
935:
872:
867:
823:
818:
812:when complete.
783:
777:
689:
688:
677:
676:
672:
671:(equivalent to
661:
660:
631:
623:mass production
592:low Earth orbit
568:
525:Propellant mass
468:Propellant mass
411:Propellant mass
354:Propellant mass
260:
256:Electron rocket
171:low Earth orbit
112:
111:
100:
99:
96:Cost per launch
59:
39:
28:
23:
22:
15:
12:
11:
5:
6073:
6063:
6062:
6057:
6052:
6047:
6030:
6029:
6027:
6026:
6021:
6016:
6011:
6005:
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6001:
5999:
5998:
5993:
5988:
5982:
5976:
5974:
5970:
5969:
5967:
5966:
5961:
5956:
5951:
5949:AgniKul Cosmos
5946:
5941:
5936:
5931:
5925:
5923:
5919:
5918:
5916:
5915:
5909:
5907:
5903:
5902:
5900:
5899:
5894:
5889:
5884:
5879:
5873:
5871:
5870:Communications
5867:
5866:
5864:
5863:
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5853:
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5843:
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5833:
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5823:
5817:
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5808:
5807:
5806:
5805:
5796:
5795:
5790:
5784:
5782:
5776:
5775:
5772:
5771:
5769:
5768:
5762:
5760:
5759:In development
5756:
5755:
5753:
5752:
5747:
5742:
5736:
5734:
5727:
5723:
5722:
5719:
5718:
5716:
5715:
5710:
5704:
5702:
5698:
5697:
5695:
5694:
5689:
5683:
5681:
5680:In development
5677:
5676:
5674:
5673:
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5671:
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5656:
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5508:
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5018:
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4695:
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4407:
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4026:
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4019:
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4009:
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3994:
3993:
3992:
3987:
3982:
3977:
3972:
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3897:
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3808:
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3791:
3781:
3776:
3771:
3766:
3761:
3756:
3751:
3746:
3741:
3735:
3733:
3732:In development
3729:
3728:
3726:
3725:
3724:
3723:
3713:
3711:Vulcan Centaur
3708:
3707:
3706:
3696:
3691:
3686:
3681:
3676:
3675:
3674:
3669:
3664:
3654:
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3404:
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3313:
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3310:
3309:
3304:
3298:
3295:
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3287:
3286:
3279:
3272:
3264:
3258:
3257:
3243:
3242:External links
3240:
3237:
3236:
3210:
3184:
3158:
3125:
3099:
3065:
3039:
3013:
2979:
2946:
2913:
2890:
2867:
2845:
2820:
2786:
2758:
2751:) – via
2732:
2725:) – via
2706:
2676:
2651:
2619:
2598:
2570:
2542:
2516:
2490:
2456:
2430:
2406:
2388:
2351:
2318:
2296:
2262:
2223:
2180:
2141:
2114:
2084:
2062:
2037:
2014:
1989:
1970:
1956:on 5 June 2020
1935:
1919:
1889:
1863:
1841:
1819:
1790:
1762:
1733:
1700:
1674:
1646:
1620:
1592:
1567:
1542:
1530:
1494:
1455:
1421:
1399:
1360:
1339:
1317:
1288:
1264:
1240:
1214:
1213:
1211:
1208:
1207:
1206:
1201:
1196:
1191:
1186:
1181:
1175:
1174:
1160:
1146:
1130:
1127:
1124:
1123:
1120:
1117:
1114:
1111:
1107:
1106:
1103:
1100:
1097:
1094:
1088:
1087:
1085:
1079:
1078:
1072:
1066:
1060:
1053:
1048:
1045:
1042:
1041:
1037:
1034:
1031:
1030:
1029:
1028:
1026:
1023:
1015:
1012:
979:
976:
934:
931:
882:microsatellite
871:
868:
866:
863:
822:
819:
817:
814:
779:Main article:
776:
773:
772:
771:
764:
761:
752:
751:
748:
745:
630:
627:
570:
569:
562:
559:
558:
555:
554:
542:
538:
537:
534:
530:
529:
526:
522:
521:
518:
514:
513:
509:
508:
501:
497:
496:
493:
489:
488:
485:
484:Maximum thrust
481:
480:
477:
473:
472:
469:
465:
464:
461:
457:
456:
452:
451:
444:
440:
439:
436:
432:
431:
430:234.2 kN (vac)
428:
427:Maximum thrust
424:
423:
420:
416:
415:
412:
408:
407:
404:
400:
399:
395:
394:
387:
383:
382:
379:
375:
374:
373:2,496 kN (vac)
371:
370:Maximum thrust
367:
366:
363:
359:
358:
355:
351:
350:
347:
343:
342:
338:
337:
334:
333:
330:
326:
325:
318:
314:
313:
310:
306:
305:
302:
298:
297:
292:
291:Total launches
288:
287:
279:
275:
274:
271:
267:
266:
265:Launch history
262:
261:
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97:
93:
92:
89:
85:
84:
75:
71:
70:
65:
61:
60:
54:
26:
9:
6:
4:
3:
2:
6072:
6061:
6058:
6056:
6053:
6051:
6048:
6046:
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6042:
6040:
6025:
6022:
6020:
6017:
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6003:
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5992:
5989:
5986:
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5908:
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5868:
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5849:
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5842:
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5804:
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5777:
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5751:
5748:
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5724:
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5711:
5709:
5706:
5705:
5703:
5699:
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5690:
5688:
5685:
5684:
5682:
5678:
5670:
5667:
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5650:
5648:
5645:
5641:
5638:
5637:
5636:
5633:
5629:
5626:
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5611:
5608:
5606:
5602:
5595:
5592:
5588:
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5584:
5583:
5582:
5578:
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5569:
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5559:
5558:
5556:
5552:
5545:
5542:
5539:
5536:
5534:
5531:
5528:
5525:
5522:
5521:Chandrayaan-4
5519:
5515:
5513:
5509:
5507:
5505:
5501:
5500:
5499:
5498:Chandrayaan-3
5496:
5492:
5490:
5486:
5484:
5482:
5478:
5477:
5476:
5475:Chandrayaan-2
5473:
5469:
5466:
5465:
5464:
5463:Chandrayaan-1
5461:
5460:
5458:
5452:
5445:
5442:
5440:
5437:
5435:
5432:
5430:
5427:
5426:
5424:
5420:
5414:
5411:
5409:
5406:
5404:
5401:
5399:
5396:
5394:
5391:
5389:
5386:
5384:
5381:
5379:
5376:
5374:
5371:
5370:
5368:
5364:
5358:
5355:
5353:
5350:
5348:
5345:
5343:
5340:
5338:
5335:
5331:
5328:
5327:
5326:
5323:
5321:
5318:
5316:
5313:
5311:
5308:
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5303:
5301:
5298:
5297:
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5286:
5276:
5273:
5271:
5268:
5266:
5263:
5261:
5258:
5256:
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5251:
5248:
5246:
5243:
5241:
5238:
5236:
5233:
5231:
5228:
5226:
5223:
5222:
5220:
5218:Organisations
5216:
5210:
5207:
5206:
5203:
5199:
5194:
5185:
5180:
5178:
5173:
5171:
5166:
5165:
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5149:
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5145:
5142:
5136:
5133:
5131:
5128:
5126:
5123:
5121:
5118:
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5113:
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5110:
5106:
5098:
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5041:
5040:
5039:
5036:
5034:
5031:
5027:
5024:
5022:
5019:
5017:
5014:
5012:
5011:UR-500 Proton
5009:
5008:
5007:
5004:
5000:
4997:
4995:
4992:
4990:
4987:
4985:
4982:
4981:
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4955:
4953:
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4916:
4913:
4911:
4908:
4907:
4906:
4903:
4899:
4896:
4894:
4891:
4887:
4884:
4882:
4879:
4878:
4877:
4874:
4870:
4867:
4865:
4862:
4860:
4857:
4856:
4855:
4852:
4848:
4845:
4843:
4840:
4839:
4838:
4835:
4833:
4830:
4829:
4828:
4825:
4823:
4820:
4818:
4815:
4813:
4810:
4808:
4805:
4803:
4800:
4798:
4797:Space Shuttle
4795:
4793:
4790:
4786:
4783:
4781:
4778:
4777:
4776:
4773:
4769:
4766:
4764:
4761:
4759:
4756:
4754:
4751:
4749:
4746:
4744:
4741:
4739:
4736:
4734:
4731:
4729:
4726:
4724:
4721:
4719:
4716:
4714:
4711:
4709:
4706:
4704:
4701:
4699:
4698:Blue Scout II
4696:
4694:
4691:
4690:
4689:
4686:
4682:
4679:
4677:
4674:
4672:
4669:
4668:
4667:
4664:
4660:
4657:
4655:
4652:
4650:
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4646:
4645:
4642:
4640:
4637:
4633:
4630:
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4625:
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4623:
4620:
4614:
4611:
4609:
4606:
4604:
4601:
4599:
4596:
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4589:
4586:
4584:
4581:
4579:
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4534:
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4527:
4525:
4522:
4521:
4520:
4517:
4515:
4512:
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3387:Firefly Alpha
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1304:@businessline
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41:
37:
33:
19:
5954:Dhruva Space
5651:
5579:
5570:
5511:
5503:
5488:
5480:
4905:Thorad-Agena
4578:Soyuz/Vostok
3678:
3382:Falcon Heavy
3227:. Retrieved
3223:
3213:
3201:. Retrieved
3196:
3187:
3175:. Retrieved
3170:
3161:
3149:. Retrieved
3137:
3128:
3116:. Retrieved
3112:
3102:
3090:. Retrieved
3078:
3068:
3056:. Retrieved
3052:
3042:
3030:. Retrieved
3026:
3016:
3004:. Retrieved
2992:
2982:
2970:. Retrieved
2958:
2949:
2937:. Retrieved
2925:
2916:
2905:, retrieved
2899:
2893:
2882:, retrieved
2876:
2870:
2858:. Retrieved
2848:
2836:. Retrieved
2832:
2823:
2811:. Retrieved
2799:
2789:
2777:. Retrieved
2773:
2735:
2709:
2697:. Retrieved
2693:the original
2688:
2679:
2667:. Retrieved
2663:
2654:
2642:. Retrieved
2638:the original
2631:
2622:
2614:the original
2601:
2589:. Retrieved
2585:
2564:
2558:the original
2545:
2533:. Retrieved
2528:
2519:
2507:. Retrieved
2503:the original
2493:
2481:. Retrieved
2469:
2459:
2447:. Retrieved
2443:
2433:
2422:the original
2409:
2401:the original
2391:
2382:
2375:. Retrieved
2354:
2342:. Retrieved
2330:
2321:
2309:. Retrieved
2299:
2287:. Retrieved
2275:
2265:
2257:
2250:. Retrieved
2243:the original
2238:
2226:
2216:
2214:
2207:. Retrieved
2200:the original
2195:
2183:
2175:
2168:. Retrieved
2161:the original
2156:
2144:
2136:
2130:the original
2117:
2105:. Retrieved
2101:the original
2096:
2087:
2075:. Retrieved
2065:
2053:. Retrieved
2049:
2040:
2029:, retrieved
2024:
2017:
2005:. Retrieved
2001:
1992:
1984:
1979:
1973:
1965:
1958:. Retrieved
1951:the original
1938:
1928:
1922:
1913:
1906:. Retrieved
1902:
1892:
1880:. Retrieved
1875:
1866:
1854:. Retrieved
1844:
1832:. Retrieved
1822:
1810:. Retrieved
1805:
1781:. Retrieved
1775:
1765:
1753:. Retrieved
1749:
1724:. Retrieved
1720:the original
1713:
1703:
1691:. Retrieved
1687:
1677:
1665:. Retrieved
1658:
1649:
1637:. Retrieved
1611:. Retrieved
1605:
1595:
1583:. Retrieved
1570:
1558:. Retrieved
1554:
1545:
1533:
1521:. Retrieved
1485:. Retrieved
1478:the original
1448:– via
1442:. Retrieved
1412:. Retrieved
1402:
1390:. Retrieved
1351:. Retrieved
1342:
1330:. Retrieved
1320:
1308:. Retrieved
1303:
1279:. Retrieved
1258:
1231:. Retrieved
1227:
1218:
1143:India portal
1008:
989:
972:
964:
952:
920:
916:
912:
897:
894:
887:
860:
857:
849:
846:
839:
824:
795:
784:
754:
753:
737:
736:
729:
717:
701:
654:
615:
608:
579:
575:
573:
487:160 kN (vac)
317:First flight
278:Launch sites
74:Manufacturer
40:
5939:Sisir Radar
5660:Suborbital
5352:Chandrayaan
4395:LauncherOne
4346:Kaituozhe-1
4123:Black Arrow
3875:Orbex Prime
3774:Hyperbola-2
3739:Antares 330
3439:Kaituozhe 2
3412:Hyperbola-1
3171:India Today
2531:(in Telugu)
2397:"NSSS 2016"
2239:isro.gov.in
2196:isro.gov.in
2157:isro.gov.in
2097:isro.gov.in
2031:2 September
2007:2 September
2002:twitter,com
1882:21 December
1852:. Frontline
1834:2 September
1783:2 September
1755:2 September
1715:Spaceflight
1667:14 February
1392:20 December
1353:2 September
1096:Successful
959:AzaadiSAT-2
835:S. Somanath
825:In 2015, a
821:Development
787:Sriharikota
329:Last flight
301:Success(es)
201:Payload to
169:Payload to
6039:Categories
5780:Spaceports
5596:(proposed)
5546:(proposed)
5540:(proposed)
5529:(proposed)
5523:(upcoming)
5446:(proposed)
5444:AstroSat-2
5366:Satellites
5293:Programmes
4400:Long March
4304:Feng Bao 1
3917:Tianlong-3
3843:New Line 1
3801:Long March
3749:Cyclone-4M
3689:Tianlong-2
3667:2.1b / STB
3662:2.1a / STA
3605:Pegasus XL
3471:Long March
3444:Kinetica 1
3367:Chollima-1
2779:5 February
2529:eenadu.net
2344:25 January
2307:. The Wire
2252:30 October
2209:30 October
2170:30 October
2107:30 October
2077:30 October
1585:30 January
1560:9 December
1523:5 November
1281:31 January
1210:References
806:Tamil Nadu
711:(SLV) and
541:Propellant
533:Powered by
500:Propellant
476:Powered by
443:Propellant
419:Powered by
386:Propellant
362:Powered by
309:Failure(s)
241:Minotaur I
234:Comparable
5964:TeamIndus
5944:Satellize
5581:Gaganyaan
5454:Lunar and
5434:Aditya-L1
5413:Kalpana-1
5378:Aryabhata
4499:Paektusan
4128:Conestoga
3885:Red Dwarf
3838:New Glenn
3769:Gravity-2
3759:Epsilon S
3392:Gravity-1
3229:17 August
3203:21 August
3177:27 August
3151:16 August
3146:0971-8257
3118:16 August
3092:16 August
3087:0971-751X
3079:The Hindu
3058:16 August
3032:16 August
3006:16 August
3001:0971-751X
2993:The Hindu
2972:16 August
2967:0013-0389
2939:16 August
2934:0971-8257
2813:12 August
2808:0971-751X
2800:The Hindu
2478:0971-751X
2470:The Hindu
2339:0971-751X
2331:The Hindu
2311:8 January
2289:17 August
2284:0971-8257
1908:31 August
1876:The Hindu
1812:16 August
1806:Firstpost
1639:7 October
1414:16 August
1332:13 August
947:cleanroom
904:AzaadiSAT
796:This new
650:SDSC-SHAR
492:Burn time
435:Burn time
378:Burn time
164:Capacity
5985:SAGA-220
5640:Launches
5628:Launches
5619:Orbital
5429:Astrosat
5330:Cartosat
5300:Bhaskara
5043:original
5033:Vanguard
5016:Proton-K
4989:original
4837:Ablestar
4822:Terran 1
4780:original
4639:Rocket 3
4546:original
4356:original
4282:Falcon 9
4277:Falcon 1
4233:IV Heavy
3949:Zuljanah
3912:Terran R
3895:Block 1B
3880:Pallas-1
3784:Kuaizhou
3744:Bloostar
3684:Starship
3635:Shavit 2
3620:Qaem 100
3610:Proton-M
3568:Minotaur
3449:Kuaizhou
3372:Electron
3340:Ariane 6
3224:The Week
3027:The Week
2907:8 August
2884:8 August
2860:8 August
2838:7 August
2833:The Wire
2699:7 August
2669:15 March
2644:14 March
2591:23 March
2535:23 March
2509:14 March
2483:20 March
2449:20 March
2377:21 March
2368:Archived
1960:6 August
1726:6 August
1693:7 August
1487:4 August
1444:1 August
1383:Archived
1233:7 August
1129:See also
1102:Failure
715:(ASLV).
517:Diameter
460:Diameter
403:Diameter
346:Diameter
251:Kuaizhou
209:Altitude
177:Altitude
140:Diameter
64:Function
5996:RESPOND
5973:Related
5766:SCE-200
5726:Engines
5701:Retired
5512:Pragyan
5489:Pragyan
5108:Classes
4979:Tsyklon
4817:Start-1
4588:Voskhod
4583:Sputnik
4519:Molniya
4504:Pilot-2
4341:Juno II
4255:Epsilon
4250:Energia
4240:Diamant
4116:Centaur
3965:Antares
3958:Retired
3907:Soyuz-7
3900:Block 2
3833:Neutron
3823:Miura 5
3657:Soyuz-2
3650:Block 1
3640:Simorgh
3417:Jielong
3345:Atlas V
3316:Current
2753:Twitter
2727:Twitter
1856:23 July
1613:19 July
1450:Twitter
1310:28 July
1093:Decade
1077:Planned
1071:Success
1059:Failure
978:SSLV-D3
933:SSLV-D2
890:SSLV-D1
870:SSLV-D1
816:History
725:delta-v
666:169.07
638:SSLV-D2
582:) is a
503:Solid (
495:106.9 s
446:Solid (
438:113.1 s
389:Solid (
246:Start-1
5929:Pixxel
5740:CE-7.5
5733:Active
5664:Rohini
5613:Active
5572:SRE-II
5506:lander
5504:Vikram
5483:lander
5481:Vikram
5439:XPoSat
5383:HAMSAT
5342:Rohini
5092:Zhuque
5026:Strela
4984:R-36-O
4927:II GLV
4915:SLV-2H
4910:SLV-2G
4898:DSV-2U
4876:Burner
4812:SS-520
4807:Sparta
4775:Shavit
4666:Saturn
4627:Shtil'
4593:Vostok
4536:Polyot
4494:Naro-1
4383:Lambda
4351:Kosmos
4336:Juno I
4260:Europa
4034:Athena
3997:Ariane
3937:Zhuque
3927:Vega E
3779:Irtysh
3716:Zhuque
3434:KAIROS
3323:Angara
3144:
3085:
2999:
2965:
2932:
2806:
2476:
2337:
2282:
2055:5 June
1551:"SSLV"
1110:2020s
1105:Total
1075:
1069:
1063:
1057:
992:EOS-08
955:EOS-07
943:EOS-07
900:EOS 02
879:EOS-02
642:EOS-07
600:rocket
552:Liquid
507:based)
450:based)
393:based)
381:94.3 s
320:03:48
273:Active
270:Status
156:Stages
132:Height
5750:Vikas
5745:CE-20
5566:SRE-1
5514:rover
5491:rover
5403:SARAL
5398:NISAR
5388:IMS-1
5373:APPLE
5347:SROSS
5337:RISAT
5320:IRNSS
5315:INSAT
5305:GAGAN
5055:Zenit
5050:VLS-1
5021:Rokot
4922:Titan
4893:Delta
4854:Agena
4802:SPARK
4688:Scout
4644:Safir
4632:Volna
4541:Soyuz
4331:H-IIB
4245:Dnepr
4133:Delta
4111:Agena
4101:SLV-3
4096:LV-3B
4051:Atlas
3625:Qased
3600:OS-M1
3402:H-IIA
3350:Ceres
2749:Tweet
2723:Tweet
2610:(PDF)
2561:(PDF)
2554:(PDF)
2425:(PDF)
2418:(PDF)
2371:(PDF)
2364:(PDF)
2246:(PDF)
2235:(PDF)
2203:(PDF)
2192:(PDF)
2164:(PDF)
2153:(PDF)
2133:(PDF)
2126:(PDF)
1954:(PDF)
1947:(PDF)
1579:(PDF)
1481:(PDF)
1474:(PDF)
1438:Tweet
1386:(PDF)
1379:(PDF)
1255:(PDF)
968:NavIC
696:crore
684:crore
668:crore
563:[
463:1.7 m
188:45.0°
119:crore
107:crore
91:India
5713:ASLV
5692:NGLV
5652:SSLV
5647:LVM3
5635:GSLV
5623:PSLV
5587:CARE
5310:GSAT
5080:3SLB
5038:Vega
4967:CT-3
4952:IIIE
4947:IIID
4942:IIIC
4937:IIIB
4932:IIIA
4832:Able
4827:Thor
4728:X-2B
4718:X-3M
4708:X-2M
4622:R-29
4514:Luna
4489:N-II
4467:3SII
4366:2/2I
4326:H-II
4314:Mk I
4309:GSLV
4292:v1.1
4287:v1.0
4213:5000
4208:4000
4203:3000
4198:2000
4193:1000
4188:0100
4106:Able
4029:ASLV
3990:230+
3932:Zero
3858:OS-M
3853:Nova
3848:NGLV
3764:Eris
3754:Deca
3699:Vega
3694:Unha
3679:SSLV
3672:2-1v
3615:PSLV
3595:Nuri
3563:LVM3
3496:3B/E
3397:GSLV
3231:2024
3205:2024
3179:2024
3153:2024
3142:ISSN
3120:2024
3094:2024
3083:ISSN
3060:2024
3034:2024
3008:2024
2997:ISSN
2974:2024
2963:ISSN
2941:2024
2930:ISSN
2909:2022
2886:2022
2862:2022
2840:2022
2815:2022
2804:ISSN
2781:2023
2701:2022
2671:2022
2646:2022
2633:ISRO
2593:2021
2537:2021
2511:2022
2485:2022
2474:ISSN
2451:2022
2379:2022
2346:2020
2335:ISSN
2313:2020
2291:2024
2280:ISSN
2254:2019
2211:2019
2172:2019
2109:2019
2079:2019
2057:2023
2033:2018
2009:2018
1962:2022
1910:2022
1884:2018
1858:2021
1836:2018
1814:2024
1785:2018
1757:2018
1728:2019
1695:2022
1669:2023
1641:2020
1615:2022
1587:2019
1562:2018
1539:SSLV
1525:2021
1489:2022
1446:2022
1416:2024
1394:2019
1355:2018
1334:2022
1312:2019
1283:2020
1235:2022
1199:LVM3
1049:2024
1046:2023
1043:2022
927:MON3
908:STEM
732:PSLV
720:HTPB
588:ISRO
580:SSLV
574:The
549:MON3
505:HTPB
448:HTPB
391:HTPB
217:Mass
193:Mass
148:Mass
127:Size
82:ISRO
78:NSIL
18:SSLV
5708:SLV
5669:ATV
5325:IRS
5075:3SL
5070:2FG
4962:23G
4957:34D
4792:SLV
4768:G-1
4763:F-1
4758:E-1
4753:A-1
4748:D-1
4743:B-1
4723:X-4
4713:X-3
4703:X-2
4693:X-1
4509:R-7
4484:N-I
4321:H-I
4223:III
4091:III
4066:E/F
3985:230
3980:130
3975:120
3970:110
3922:VLM
3890:SLS
3828:MLV
3645:SLS
3630:RS1
3556:11H
3328:1.2
2566:(…)
2217:sic
945:in
923:MMH
804:in
694:35
682:30
648:at
606:.
545:MMH
520:2 m
406:2 m
365:S85
349:2 m
322:UTC
159:3+1
117:35
105:30
6041::
5085:3F
5065:2M
4972:IV
4676:IB
4659:1B
4654:1A
4613:2M
4571:U2
4551:FG
4479:N1
4462:3S
4457:3H
4452:3C
4447:4S
4442:Mu
4435:4A
4430:3B
4420:2E
4415:2A
4410:1D
4388:4S
4376:3M
4270:II
4228:IV
4218:II
4086:II
4044:II
3816:12
3811:10
3794:31
3789:21
3578:IV
3551:11
3541:7A
3531:6A
3521:5B
3511:4C
3506:4B
3501:3C
3491:3A
3486:2F
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3476:2C
3464:11
3459:1A
3407:H3
3360:1S
3333:A5
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