533:
74:
Spin-stabilization is used on rockets and spacecraft where attitude control is required without the requirement for on-board 3-axis propulsion or mechanisms, and sensors for attitude control and pointing. On rockets with a solid motor upper stage, spin stabilization is used to keep the motor from
154:
and depended on the second stage for proper orientation prior to stage separation, but was sometimes equipped with a nutation control system to maintain proper spin axis. It also included a yo-weight system to induce tumbling in the third stage after payload separation to prevent recontact, or a
170:
With advancements in attitude control propulsion systems, guidance systems, and the needs for satellites to point instruments and communications systems precisely, 3-axis attitude control has become much more common than spin-stabilization for systems operating in space.
141:
rocket motors that were spin-stabilized in order to inject the satellites into the high-energy hyperbolic orbits necessary to achieve solar system escape velocity. Additionally, both probes were spin-stabilized during their flights and rotated at approximately 5
149:
rocket booster sits on top of spin table, and before it is separated it is spun up to stabilize it during the separation from the previous stage. The Delta II launch vehicle third stage employed a Star 48 motor and was
75:
drifting off course as they don't have their own thrusters. Usually small rockets are used to spin up the spacecraft and rocket then fire the rocket and send the craft off.
455:
503:
90:
launch vehicles used spin-stabilization. The upper stages on both system employ spin-stabilization to stabilize the system during propulsive maneuvers.
570:
425:
589:
17:
51:
594:
444:
309:
205:
563:
301:
185:
151:
116:
63:
392:
599:
253:
112:
415:
94:
31:
544:
347:
556:
227:
8:
504:"When and why did three-axis stabilization become prominent in geostationary satellites?"
105:
370:
276:
333:
421:
280:
123:
300:
268:
481:
540:
43:
583:
164:
156:
272:
134:
130:
87:
62:. For most satellite applications this approach has been superseded by
55:
482:
Theory and Design Curves for a Yo-Yo De-Spin
Mechanism for Satellites
180:
101:
83:
39:
47:
146:
138:
59:
137:
probes on two Atlas
Centaur vehicles in 1972 and 1973 employed
163:
Despinning can be achieved by various techniques, including
305:
532:
126:
was spin-stabilized and arrived at
Jupiter orbit in 2016.
50:
along the longitudinal axis. The concept originates from
119:
prior to its attempted landing on Mars in
October 2016.
104:
spacecraft, the second object sent on a lunar flyby in
159:
mechanism to slow the rotation before payload release.
115:
was spun up to 2.5 RPM before being ejected from the
417:
Space
Handbook: A War Fighter's Guide to Space, V. 1
78:
Rockets and spacecraft that use spin stabilization:
108:, maintained its attitude using spin-stabilization.
27:
Method of stabilizing a satellite or launch vehicle
334:"Schiaparelli EDM – ExoMars | Spaceflight101"
58:, where the spin is commonly obtained by means of
581:
484:(Report). Defense Technical Information Center
564:
294:
261:Proceedings of the Indian Academy of Sciences
228:"Minotaur V High Energy Space Launch Vehicle"
420:. Government Printing Office. p. 126.
571:
557:
254:"An overview of the 'Aryabhata' project"
445:"Delta II Payload Planner's Guide 2007"
439:
437:
14:
582:
461:from the original on 19 September 2011
479:
413:
527:
434:
414:Muolo, Michael J. (November 1993).
251:
145:In operation as a third stage, the
24:
506:. Stack Exchange Space Exploration
25:
611:
368:
97:satellite used spin-stabilization
531:
52:conservation of angular momentum
496:
473:
480:Fedor, J.V. (August 1, 1961).
407:
385:
362:
340:
326:
245:
220:
198:
13:
1:
191:
38:is a method of stabilizing a
543:. You can help Knowledge by
7:
590:Spacecraft attitude control
539:This rocketry article is a
174:
10:
616:
526:
348:"Juno Spacecraft Presskit"
252:Rao, UR (September 1978).
310:The Moon Probe Pioneer IV
302:Jet Propulsion Laboratory
186:Spin-stabilized satellite
117:ExoMars Trace Gas Orbiter
64:three-axis stabilization
113:Schiaparelli EDM lander
46:by means of spin, i.e.
595:Spaceflight technology
393:"The Pioneer Missions"
206:"Jupiter-C/Explorer 1"
69:
373:. Gunter's Space Page
32:aerospace engineering
395:. NASA. Mar 26, 2007
304:(under contract for
371:"Pioneer 10, 11, H"
315:(Report). NASA-JPL
273:10.1007/BF02843538
36:spin stabilization
18:Spin-stabilisation
552:
551:
427:978-0-16-061355-5
369:Krebs, Gunter D.
16:(Redirected from
607:
573:
566:
559:
535:
528:
516:
515:
513:
511:
500:
494:
493:
491:
489:
477:
471:
470:
468:
466:
460:
449:
441:
432:
431:
411:
405:
404:
402:
400:
389:
383:
382:
380:
378:
366:
360:
359:
357:
355:
344:
338:
337:
330:
324:
323:
321:
320:
314:
298:
292:
291:
289:
287:
258:
249:
243:
242:
240:
238:
232:
224:
218:
217:
215:
213:
202:
129:The launches of
21:
615:
614:
610:
609:
608:
606:
605:
604:
580:
579:
578:
577:
524:
520:
519:
509:
507:
502:
501:
497:
487:
485:
478:
474:
464:
462:
458:
447:
443:
442:
435:
428:
412:
408:
398:
396:
391:
390:
386:
376:
374:
367:
363:
353:
351:
346:
345:
341:
332:
331:
327:
318:
316:
312:
299:
295:
285:
283:
256:
250:
246:
236:
234:
230:
226:
225:
221:
211:
209:
204:
203:
199:
194:
177:
152:spin-stabilized
72:
28:
23:
22:
15:
12:
11:
5:
613:
603:
602:
600:Rocketry stubs
597:
592:
576:
575:
568:
561:
553:
550:
549:
536:
518:
517:
495:
472:
433:
426:
406:
384:
361:
339:
325:
293:
267:(2): 117–133.
244:
219:
196:
195:
193:
190:
189:
188:
183:
176:
173:
161:
160:
143:
127:
120:
109:
98:
91:
71:
68:
54:as applied to
44:launch vehicle
26:
9:
6:
4:
3:
2:
612:
601:
598:
596:
593:
591:
588:
587:
585:
574:
569:
567:
562:
560:
555:
554:
548:
546:
542:
537:
534:
530:
529:
525:
522:
505:
499:
483:
476:
457:
453:
452:ulalaunch.com
446:
440:
438:
429:
423:
419:
418:
410:
394:
388:
372:
365:
349:
343:
335:
329:
311:
307:
303:
297:
282:
278:
274:
270:
266:
262:
255:
248:
229:
223:
208:. NASA NSSDCA
207:
201:
197:
187:
184:
182:
179:
178:
172:
168:
166:
165:yo-yo de-spin
158:
157:yo-yo de-spin
153:
148:
144:
140:
136:
132:
128:
125:
121:
118:
114:
110:
107:
103:
99:
96:
92:
89:
85:
81:
80:
79:
76:
67:
65:
61:
57:
53:
49:
45:
41:
37:
33:
19:
545:expanding it
538:
523:
521:
508:. Retrieved
498:
486:. Retrieved
475:
463:. Retrieved
451:
416:
409:
397:. Retrieved
387:
375:. Retrieved
364:
354:December 31,
352:. Retrieved
342:
328:
317:. Retrieved
296:
284:. Retrieved
264:
260:
247:
235:. Retrieved
222:
210:. Retrieved
200:
169:
162:
77:
73:
35:
29:
584:Categories
510:January 1,
488:January 1,
399:January 1,
377:January 1,
319:2017-02-26
308:) (1959).
286:January 1,
237:January 1,
212:January 1,
192:References
135:Pioneer 11
131:Pioneer 10
88:Minotaur V
56:ballistics
281:128455319
181:Gyroscope
102:Pioneer 4
95:Aryabhata
84:Jupiter-C
40:satellite
456:Archived
175:See also
48:rotation
465:24 July
147:Star 48
139:Star 37
60:rifling
424:
350:. NASA
279:
233:. NASA
459:(PDF)
448:(PDF)
313:(PDF)
277:S2CID
257:(PDF)
231:(PDF)
541:stub
512:2023
490:2023
467:2014
422:ISBN
401:2023
379:2023
356:2022
306:NASA
288:2023
239:2023
214:2023
142:rpm.
133:and
124:Juno
122:The
111:The
106:1959
100:The
93:The
86:and
82:The
269:doi
70:Use
42:or
30:In
586::
454:.
450:.
436:^
275:.
265:C1
263:.
259:.
167:.
66:.
34:,
572:e
565:t
558:v
547:.
514:.
492:.
469:.
430:.
403:.
381:.
358:.
336:.
322:.
290:.
271::
241:.
216:.
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.