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Reaction wheel

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not continue. Although the failed reaction wheels still function, they are experiencing friction exceeding acceptable levels, and consequently hindering the ability of the telescope to properly orient itself. The Kepler telescope was returned to its "point rest state", a stable configuration that uses small amounts of thruster fuel to compensate for the failed reaction wheels, while the Kepler team considered alternative uses for Kepler that do not require the extreme accuracy in its orientation needed by the original mission. On May 16, 2014, NASA extended the Kepler mission to a new mission named
287:. When mounted to a rigid spacecraft, applying a constant torque to the wheel using one of the gimbal motors causes the spacecraft to develop a constant angular velocity about a perpendicular axis, thus allowing control of the spacecraft's pointing direction. CMGs are generally able to produce larger sustained torques than RWs with less motor heating, and are preferentially used in larger or more-agile (or both) spacecraft, including 28: 20: 122:(better known as torque rods), which transfer angular momentum to the Earth through its planetary magnetic field requiring only electrical power and no fuel. They are however limited to areas of space with a sufficiently large magnetic field (such as in low Earth orbit). In the absence of a sufficiently strong magnetic field, the next most efficient practice is to use high-efficiency attitude jets such as 85:. Doing so alters the spacecraft's rotational dynamics so that disturbance torques perpendicular to one axis of the satellite (the axis parallel to the wheel's spin axis) do not result directly in spacecraft angular motion about the same axis as the disturbance torque; instead, they result in (generally smaller) angular motion ( 240:
ability to maintain a sufficiently precise orientation to continue its original mission. On August 15, 2013, engineers concluded that Kepler's reaction wheels cannot be recovered and that planet-searching using the transit method (measuring changes in star brightness caused by orbiting planets) could
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For three-axis control, reaction wheels must be mounted along at least three directions, with extra wheels providing redundancy to the attitude control system. A redundant mounting configuration could consist of four wheels along tetrahedral axes, or a spare wheel carried in addition to a three axis
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Over time, reaction wheels may build up enough stored momentum to exceed the maximum speed of the wheel, called saturation. However, slowing down the wheels imparts a torque causing undesired rotation. Designers therefore supplement reaction wheel systems with other attitude control mechanisms to
89:) of that spacecraft axis about a perpendicular axis. This has the effect of tending to stabilize that spacecraft axis to point in a nearly-fixed direction, allowing for a less-complicated attitude control system. Satellites using this "momentum-bias" stabilization approach include 114:
cancel out the torque caused by "desaturating" the reaction wheels. Typically designers use "reaction control systems"; arrays of small chemical rocket engines that fire as the wheels slow down to counter the torque the wheels are imparting on the spacecraft as they slow down.
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to briefly delay its departure from Vesta's gravity until September 5, 2012, and it planned to use thruster jets instead of the reaction wheels during the three-year journey to Ceres. The loss of the reaction wheels limited the camera observations on the approach to Ceres.
271:'s reaction wheels caused the mission control team to power off the suspected wheel, putting the observatory in safe mode as a precaution. This was the first time a reaction wheel failed on Swift in 17 years. Swift resumed science operations on February 17, 2022. 206:) replaced one after 'electrical anomalies', rather than any mechanical problem. Study of the returned mechanism provided a rare opportunity to study equipment that had undergone long-term service (seven years) in space, particularly for the effects of vacuum on 102:
configuration. Changes in speed (in either direction) are controlled electronically by computer. The strength of the materials used in a reaction wheel determine the speed at which the wheel would come apart, and therefore how much angular momentum it can store.
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More fuel efficient methods for reaction wheel desaturation have been developed over time. By reducing the amount of fuel the spacecraft needs to be launched with, they increase the useful payload that can be delivered to orbit. These methods include
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had excess friction in one reaction wheel in June 2010. It was originally scheduled to depart Vesta and begin its two-and-a-half-year journey to Ceres on August 26, 2012; however, a problem with another of the spacecraft's reaction wheels forced
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The failure of one or more reaction wheels can cause a spacecraft to lose its ability to maintain attitude (orientation) and thus potentially cause a mission failure. Recent studies conclude that these failures can be correlated with
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Since the reaction wheel is a small fraction of the spacecraft's total mass, easily controlled, temporary changes in its speed result in small changes in angle. The wheels therefore permit very precise changes in a spacecraft's
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needed for fuel.. They provide a high pointing accuracy, and are particularly useful when the spacecraft must be rotated by very small amounts, such as keeping a telescope pointed at a star.
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replaced another reaction wheel. Neither of these wheels had failed and Hubble was designed with four redundant wheels, and maintained pointing ability so long as three were functional.
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technique to save fuel. Since its fourth maneuver in its elliptical orbit, to prevent shakes when the amount of liquid fuel ran low, there was a need to use a reaction wheel.
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spacecraft, an X-axis reaction wheel failed. The Y-axis wheel failed in 2005, causing the craft to rely on chemical thrusters to maintain attitude control.
850: 893: 663: 93:; by orienting the momentum wheel's axis to be parallel to the orbit-normal vector, this satellite is in a "pitch momentum bias" configuration. 81:
A reaction wheel is sometimes operated at a constant (or near-constant) rotation speed, to provide a satellite with a large amount of stored
488: 43:) is an electric motor attached to a flywheel, which, when its rotation speed is changed, causes a counter-rotation proportionately through 500: 686: 283:(CMG) is a related but different type of attitude actuator, generally consisting of a momentum wheel mounted in a one-axis or two-axis 822: 249:. On October 30, 2018, NASA announced the end of the Kepler mission after it was determined that the fuel supply had been exhausted. 638: 166:. LightSail 2 uses a reaction wheel system to change orientation by very small amounts, allowing it to receive different amounts of 760: 471: 31:
A momentum/reaction wheel comprising part of a high-accuracy Conical Earth Sensor to maintain a satellite's precise attitude
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Spacecraft Gyroscopes And Reaction Wheels. You Can Never Have Enough | Fraser Cain | Universe Today | Aug, 2019
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Astronauts replaced one of the four Reaction Wheel Assemblies that make up Hubble's Pointing Control System.
403: 210:. The lubricating compound was found to be in 'excellent condition'. In 2002, during Servicing Mission 3B ( 530: 429: 296: 107: 63: 875: 153: 550:
Carré, D. J.; Bertrand, P. A. (1999). "Analysis of Hubble Space Telescope Reaction Wheel Lubricant".
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A Newly Discovered Branch of the Fault Tree Explaining Systemic Reaction Wheel Failures And Anomalies
110:. For this reason, reaction wheels are often used to aim spacecraft carrying cameras or telescopes. 280: 314: 514: 187:
effects. These events probably caused failures by inducing electrostatic discharge in the steel
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have replaced a reaction wheel. In February 1997, the Second Servicing Mission (
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Markley, F. Landis; Reid G. Reynolds; Frank X. Liu; Kenneth L. Lebsock (2009).
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On the evening of Tuesday, January 18, 2022, a possible failure of one of the
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From July 2012 to May 11, 2013, two out of the four reaction wheels in the
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rocket on 22 February 2019 1:45 UTC, with the goal of landing on the
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has six reaction wheels built by Rockwell Collins Deutschland.
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was launched on 25 June 2019, focused around the concept of a
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NASA News, February 18, 2022, NASA. Retrieved April 16, 2023
853:. NASA / Jet Propulsion Laboratory. Archived from 795: 611: 142: 892:
Sinclair, Doug; Grant, C. Cordell; Zee, Robert E. (2007).
531:"Team Hubble: Servicing Missions -- Servicing Mission 3B" 292: 51:; it is not capable of moving from one place to another ( 786:
Sobeck, Charlie (May 16, 2014). Johnson, Michele (ed.).
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wheels, compromising the smoothness of the mechanism.
540: 406:. Universität Stuttgart Institut fĂĽr Raumfahrtsysteme 687:"NASA's Kepler Mended, but May Never Fully Recover" 876:NASA's NASA's Swift Observatory Returns to Science 525: 523: 378:Wiley J Larson and James R Wertz (January 1999). 174:across the sail, resulting in a higher altitude. 932: 844: 842: 520: 472:"spaceil-conducts-another-successful-maneuver" 177: 47:. A reaction wheel can rotate only around its 779: 656: 549: 839: 678: 454:"israels-moon-mission-launched-successfully" 329: â€“ Method used to accelerate spacecraft 706: 236:failed. This loss severely affected Kepler 16:Attitude control device used in spacecraft 636: 427: 26: 23:A small reaction wheel viewed in profile 18: 684: 933: 851:"Dawn Engineers Assess Reaction Wheel" 785: 373: 371: 369: 367: 365: 58:Reaction wheels are used primarily by 905:"Reaction Wheel at Wolfram Research" 849:Cook, Jia-Rui C. (August 18, 2012). 848: 820: 712: 423: 421: 685:Overbye, Dennis (August 15, 2013). 362: 223:In 2004, during the mission of the 13: 758: 274: 14: 962: 885: 802:from the original on May 17, 2014 552:Journal of Spacecraft and Rockets 418: 380:Space Mission Analysis and Design 323: â€“ Satellite X-ray telescope 926:from the original on 2022-10-09. 45:conservation of angular momentum 869: 814: 752: 734: 630: 600: 578: 382:(3 ed.). Microcosm Press. 214:), astronauts from the shuttle 713:Wall, Mike (August 15, 2013). 507: 493: 482: 464: 446: 396: 340: 311: â€“ Aerospace manufacturer 198:Two servicing missions to the 1: 333: 821:Chou, Felicia (2018-10-30). 7: 941:Spacecraft attitude control 302: 297:International Space Station 178:Failures and mission impact 129: 70:or external applicators of 10: 967: 637:Mike Wall (May 15, 2013). 154:James Webb Space Telescope 348:"Reaction/Momentum Wheel" 96: 281:control moment gyroscope 513:W. Bialke, E. Hansell " 315:Reaction control system 234:Kepler space telescope 200:Hubble Space Telescope 32: 24: 946:Spacecraft propulsion 327:Spacecraft propulsion 252:The NASA space probe 145:. Beresheet uses the 66:, and do not require 30: 22: 74:, which reduces the 564:1999JSpRo..36..109C 460:. 22 February 2019. 147:low-energy transfer 53:translational force 404:"Attitude Control" 137:was launched on a 33: 25: 857:on March 15, 2015 748:. 16 August 2013. 666:. August 15, 2013 430:"Control Devices" 309:Collins Aerospace 269:Swift Observatory 958: 927: 925: 918: 908: 900: 898: 879: 873: 867: 866: 864: 862: 846: 837: 836: 834: 833: 818: 812: 811: 809: 807: 783: 777: 776: 774: 772: 756: 750: 749: 738: 732: 731: 729: 727: 710: 704: 703: 701: 699: 682: 676: 675: 673: 671: 660: 654: 653: 651: 649: 634: 628: 627: 625: 623: 614:. Archived from 604: 598: 597: 595: 593: 582: 576: 575: 547: 538: 537: 527: 518: 511: 505: 504: 497: 491: 486: 480: 479: 478:. 19 March 2019. 468: 462: 461: 450: 444: 443: 441: 440: 425: 416: 415: 413: 411: 400: 394: 393: 375: 360: 359: 357: 355: 344: 239: 83:angular momentum 64:attitude control 966: 965: 961: 960: 959: 957: 956: 955: 931: 930: 923: 916: 903: 896: 888: 883: 882: 874: 870: 860: 858: 847: 840: 831: 829: 819: 815: 805: 803: 784: 780: 770: 768: 759:Hunter, Roger. 757: 753: 740: 739: 735: 725: 723: 711: 707: 697: 695: 683: 679: 669: 667: 662: 661: 657: 647: 645: 635: 631: 621: 619: 618:on June 1, 2013 606: 605: 601: 591: 589: 584: 583: 579: 548: 541: 529: 528: 521: 512: 508: 503:. 21 June 2019. 499: 498: 494: 487: 483: 470: 469: 465: 452: 451: 447: 438: 436: 428:mars.nasa.gov. 426: 419: 409: 407: 402: 401: 397: 390: 376: 363: 353: 351: 346: 345: 341: 336: 305: 277: 275:Similar devices 237: 180: 132: 99: 62:for three-axis 17: 12: 11: 5: 964: 954: 953: 948: 943: 929: 928: 909: 901: 887: 886:External links 884: 881: 880: 868: 838: 813: 778: 751: 733: 705: 692:New York Times 677: 655: 629: 599: 577: 572:10.2514/2.3422 558:(1): 109–113. 539: 519: 506: 492: 481: 463: 445: 417: 395: 388: 361: 338: 337: 335: 332: 331: 330: 324: 318: 312: 304: 301: 276: 273: 179: 176: 131: 128: 98: 95: 49:center of mass 37:reaction wheel 15: 9: 6: 4: 3: 2: 963: 952: 949: 947: 944: 942: 939: 938: 936: 922: 915: 910: 906: 902: 895: 890: 889: 877: 872: 856: 852: 845: 843: 828: 824: 817: 801: 797: 793: 789: 782: 766: 762: 755: 747: 743: 737: 722: 721: 716: 709: 694: 693: 688: 681: 665: 659: 644: 640: 633: 617: 613: 609: 603: 587: 581: 573: 569: 565: 561: 557: 553: 546: 544: 536: 532: 526: 524: 516: 510: 502: 496: 489: 485: 477: 473: 467: 459: 455: 449: 435: 434:mars.nasa.gov 431: 424: 422: 405: 399: 391: 389:1-881883-10-8 385: 381: 374: 372: 370: 368: 366: 349: 343: 339: 328: 325: 322: 319: 316: 313: 310: 307: 306: 300: 298: 294: 290: 286: 282: 272: 270: 265: 262: 257: 256: 250: 248: 244: 235: 230: 228: 227: 221: 219: 218: 213: 209: 205: 201: 196: 194: 190: 189:ball bearings 186: 185:space weather 175: 173: 169: 165: 161: 157: 155: 150: 148: 144: 140: 136: 127: 125: 124:ion thrusters 121: 120:magnetorquers 115: 111: 109: 103: 94: 92: 88: 84: 79: 77: 76:mass fraction 73: 69: 65: 61: 56: 54: 50: 46: 42: 38: 29: 21: 907:. June 2008. 871: 859:. Retrieved 855:the original 830:. Retrieved 826: 816: 804:. Retrieved 791: 781: 771:24 September 769:. Retrieved 764: 754: 745: 736: 724:. Retrieved 718: 708: 696:. Retrieved 690: 680: 668:. Retrieved 658: 646:. Retrieved 632: 620:. Retrieved 616:the original 602: 590:. Retrieved 586:"Gyroscopes" 580: 555: 551: 534: 509: 495: 484: 475: 466: 457: 448: 437:. Retrieved 433: 408:. Retrieved 398: 379: 352:. 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Index



conservation of angular momentum
center of mass
translational force
spacecraft
attitude control
rockets
torque
mass fraction
angular momentum
precession
SCISAT-1
attitude
magnetorquers
ion thrusters
Beresheet
Falcon 9
Moon
low-energy transfer
James Webb Space Telescope
LightSail 2
solar sail
momentum
light
space weather
ball bearings
Ithaco
Hubble Space Telescope
STS-82

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