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Drop test

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On March 4, 2012, a C-17 dropped an Orion test article from an altitude of 25,000 feet (7,600 m). The capsule's parachutes successfully deployed between 15,000 to 20,000 feet (4,600 to 6,100 m), slowing the spacecraft to a landing on ground in the Arizona desert. The capsule landed at a
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were conducted to test the Space Shuttle's flight characteristics. Because the Space Shuttle is designed to glide unpowered during its descent and landing, a series of drop tests using a test orbiter were used to demonstrate that the orbiter could be successfully controlled in unpowered flight.
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landing systems. The airbags are located underneath the heat shield of the CST-100, which is designed to be separated from the capsule while under parachute descent at about 5,000 feet (1,500 m) altitude. The tests were carried out at ground speeds between 10 and 30 miles per hour (16 and
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to an unpowered landing or equip the orbiter with pop-out jet engines in order to make a powered landing. While powered landing design required carrying the engines and jet fuel, adding weight and complexity to the orbiter, engineers began favoring the powered landing option. In response, NASA
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to a height of ten feet and then dropped, simulating the impact of a landing at nineteen feet per second (5.8 m/s). The F6F was ultimately dropped from a height of twenty feet (6.1 m), demonstrating it could absorb twice the force of a carrier landing. Drop tests are still used in the
582:. For testing, the capsule is mounted on a pallet system and placed inside the cargo aircraft. Parachutes on the pallet are used to pull the pallet and capsule out of the rear of the aircraft; the capsule then separates from the pallet and begins its free fall descent. 127:
The landing gear on aircraft used on aircraft carriers must be stronger than those on land-based aircraft, due to higher approach speeds and sink rates during carrier landings. As early as the 1940s, drop tests were conducted by lifting a carrier-based plane such as the
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involved the release of an unpowered aircraft from a powered aircraft, these tests were not typical of drop testing because the orbiter was actually carried and released from a position above the SCA. This arrangement was potentially dangerous because it placed
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with simulated internal organs were located inside the helicopter and used to assess internal injuries from such a crash. Due to extensive damage to the test helicopter after the second test, no third test was planned.
242:, have made both unpowered drop tests and powered drop launches. Prior to powered flights using its rocket engine, the HL-10 made 11 unpowered drop flights in order to study the handling qualities and stability of the 563:
crewed capsule by repeatedly dropping an Orion test vehicle into a large water basin. The tests simulated water landings at speeds varying from 7 to 50 mph (11 to 80 km/h) by changing the height of the drop
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to an altitude of 15,000 to 30,000 feet (4,600 to 9,100 m). After a series of captive-flight tests in which the orbiter was not released, five free-flight tests were performed in August through October 1977.
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to an altitude of 11,000 feet (3,400 m) and then released; the capsule's three main parachutes then deployed successfully and slowed the capsule's descent. Immediately prior to landing, the capsule's six
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immediately after release. As a result, the "drop" was conducted by using a series of carefully planned maneuvers to minimize the risk of aircraft collision. Immediately after release, the
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In 2011 and 2012, NASA also conducted drop tests of the Orion test vehicle's parachute systems and land-based landing capabilities. In each test, the Orion spacecraft was dropped from a
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inflated underneath the capsule in order to absorb some of the impact energy from landing. Similar drop tests are planned in order to conduct additional airbag testing, as well as
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helicopter donated by the U.S. Army, NASA dropped the helicopter at an angle from an altitude of 35 feet (11 m) to simulate a hard helicopter landing. Sophisticated
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In April 2012, Boeing conducted another drop test of its CST-100 prototype space capsule in order to test the capsule's landing systems. The test vehicle was raised by
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mothership during a drop test. The pylon used to carry experimental vehicles is visible near the top of the photo, between the fuselage and inboard right engine.
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would climb to the right while the SCA performed a shallow dive to the left, allowing for quick vertical and horizontal separation between the two aircraft.
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was one of two such bombers modified to carry the X-15; while the other plane was retired in 1969 after the end of the X-15 program, NASA continued using
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48 km/h) in order to simulate cross wind conditions at the time of landing. Bigelow Aerospace built the mobile test rig and conducted the tests.
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above the basin. The range of landing velocities allowed NASA to simulate a range of possible entry and landing conditions during water landings.
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to demonstrate the feasibility of landing a lifting-body aircraft in unpowered flight. In 1975, the X-24B aircraft was dropped from a
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by Air Force pilots, following a tradition of referring to aircraft numbered with multiple zeroes as "Balls" plus the final number.
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by raising the test vehicle to a specific altitude and then releasing it. Test flights involving powered aircraft, particularly
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may be done to test the survivability of landing, primarily by testing the capsule's descent characteristics and its post-
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underwent drop tests to simulate its maximum descent rate of 26.4 feet per second (8.0 m/s) during carrier landings.
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In 2009 and 2010, NASA conducted a pair of drop tests to study the survivability of helicopter crashes. Using an
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to a target altitude for release. Low-altitude drop tests may be conducted by releasing the test vehicle from a
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in order to test the capsule's parachute systems prior to the start of manned testing of the Apollo spacecraft.
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to commit to an unpowered landing design, which would save weight and increase the orbiter's payload capacity.
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In 2011 and 2012, NASA conducted a series of short drop tests on the survivability of water landings in its
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for use in drop testing. NASA conducted a series of tests in 1964 which involved dropping BP-19A from a
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landing systems. These tests are typically carried out uncrewed prior to any human spaceflight testing.
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Back Down to Earth: The Development of Space Policy for NASA During the Jimmy Carter Administration
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were also drop tested, from altitudes of up to 45,000 feet (14,000 m), in order to study its
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testing, or other theoretical design characteristics of an aircraft or spacecraft's design.
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carried numerous experimental vehicles including the HL-10, X-24A, X-24B, X-38, and X-43A.
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before turning it over to NASA. Flying with NASA tail number 008, the plane was nicknamed
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speed of 17 mph (27 km/h), well below the designed maximum touchdown speed.
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High-altitude drop tests may be conducted by carrying the test vehicle aboard a
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of a planned or crash landing. This allows the vehicle's designers to validate
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In September 2011, Boeing conducted a series of drop tests, carried out in the
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conditions. The X-24B successfully made two unpowered precision landings at
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received significant modifications in order to carry the X-15. A special
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for drop tests until it was retired in 2004. During its 50-year career,
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Some experimental aircraft designed for airborne launches, such as the
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Orion test article after release from C-130 and separation from pallet
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of the aircraft's rockets after release from its carrier aircraft.
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in the 1970s, engineers debated whether to design the orbiter to
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of the test vehicle, to test its landing systems, or to evaluate
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descent to a landing site. Drop tests may be used to verify the
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development and testing of carrier-based aircraft; in 2010, the
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aircraft have been drop tested or drop launched. Many powered
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at an altitude of 45,000 feet (14,000 m) above the
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is a method of testing the in-flight characteristics of
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In the case of unpowered aircraft, the test vehicle
1276:"Orion spacecraft's parachutes tested over Arizona" 122: 1329:"Boeing's Space Capsule Undergoes First Drop Test" 1299:"Space capsule tests aim to ensure safe landings" 929: 1394: 1110:"Private Space Plane Poised for Big Test Flight" 215:were specifically designed to be drop launched. 452:in free flight directly in front of the SCA's 231:capabilities, and deployment of its steerable 1057: 1031:NASA - Dryden Flight Research Center (1977). 1370: 1368: 1224: 399: 804:"JSF simulated carrier landing successful" 1365: 1343: 504: 497:. The unmanned vehicle made a landing at 263:Early experimental aircraft, such as the 29:being released during airborne drop test. 1256:. NASASpaceflight.com. February 26, 2012 1166:"Testing NASA's Next Deep Space Vehicle" 550: 523: 382: 166: 139: 20: 783:"Hellcats were built to take a beating" 410:In 1977, a series of drop tests of the 335:X-24B role in Space Shuttle development 1395: 907: 892: 844: 715:. Naval History Blog. January 12, 2011 354:conducted unpowered drop tests of the 780: 755: 638: 249: 16:Method of testing aircraft/spacecraft 1296: 1290: 1232:"Future Space Flight: Orion Testing" 1351:"Chopper Drop Tests New Technology" 1303:Boeing Defense Space & Security 478:plans to conduct drop tests of its 13: 1188:"Orion Continues to Make a Splash" 1058:Damohn, Ph.D., Mark (March 2001). 1024: 899:"Fact Sheet First Generation X-1." 874:"Fact Sheets - HL-10 Lifting Body" 148:research vehicle is released from 135:Lockheed Martin F-35C Lightning II 14: 1419: 1210:"Orion Drop Test - Jan. 06, 2012" 914:"Fact Sheet Bell X-2 Starbuster." 589: 118:Aircraft and lifting-body testing 1376:"Chopper Crash Test a Smash Hit" 1331:. Popular Science. April 4, 2012 1033:"Shuttle Enterprise Free Flight" 781:Graff, Cory (December 6, 2012). 602:, to validate the design of the 546: 123:Carrier landing simulation tests 1321: 1297:Memi, Ed (September 12, 2011). 1268: 1246: 1202: 1180: 1158: 1130: 1102: 1076: 1051: 1002: 980: 958: 866: 463: 423:These drop tests, known as the 271:, were carried aboard modified 822: 806:. July 8, 2010. Archived from 796: 774: 760:. Zenith Imprint. p. 39. 749: 727: 705: 683: 661: 1: 940:"NASA's Mothership Factsheet" 655: 491:Dryden Flight Research Center 926:. Retrieved: March 26, 2013. 904:. Retrieved: March 26, 2013. 863:. Retrieved: March 26, 2013. 279:bombers. In the 1950s, the 7: 713:"First Test of Angled Deck" 443:While free-flight tests of 10: 1424: 1062:. iUniverse. p. 139. 876:. NASA.gov. Archived from 756:Graff, Cory (April 2009). 532:built BP-19A, an uncrewed 467: 406:Approach and Landing Tests 403: 338: 256: 1010:"X-24B Precision Landing" 476:Sierra Nevada Corporation 427:program, used a modified 425:Approach and Landing Test 345:During the design of the 1190:. NASA. December 2, 2011 990:. NASA.gov. July 1, 2011 856:January 7, 2022, at the 509:Drop tests of prototype 433:Shuttle Carrier Aircraft 400:Space Shuttle Enterprise 394:Shuttle Carrier Aircraft 227:and handling qualities, 75:after its release in an 56:, may be referred to as 924:NASA Dryden Fact Sheets 919:March 15, 2017, at the 902:NASA Dryden Fact Sheets 861:NASA Dryden Fact Sheets 530:North American Aviation 291:bomber to be used as a 281:United States Air Force 81:aerodynamic performance 54:rocket-powered aircraft 1035:. NASA. Archived from 556: 505:Crewed capsule testing 499:Edwards Air Force Base 396: 374:Edwards Air Force Base 163: 93:computer flight models 30: 1403:Aerospace engineering 1309:on September 24, 2011 1168:. NASA. July 22, 2011 554: 537:Apollo command module 524:Apollo command module 386: 378:Space Shuttle program 347:Space Shuttle orbiter 341:Martin Marietta X-24B 295:for the experimental 205:Orbital Sciences X-34 197:Martin Marietta X-24A 167:Experimental aircraft 143: 24: 880:on December 18, 2021 737:. globalsecurity.org 671:. December 10, 2012 370:atmospheric reentry 193:North American X-15 130:Grumman F6F Hellcat 1353:. December 8, 2009 1118:. January 30, 2013 1090:. February 4, 2013 758:F6F Hellcat at War 735:"Fighter Aircraft" 649:crash test dummies 639:Helicopter testing 557: 397: 392:being released by 164: 31: 1012:. 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Index


test article
prototype
experimental
aircraft
spacecraft
rocket-powered aircraft
launch
falls
glides
unpowered
aerodynamic performance
flight dynamics
survivability
computer flight models
wind tunnel
mothership
crane
gantry
Grumman F6F Hellcat
Lockheed Martin F-35C Lightning II

X-38
Balls 8
NASA
B-52
experimental
prototype
X-planes
Bell X-1

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