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thermal protection cowl containing the spherical propellant tank. A barrier splits the tank into two separate compartments, filled with the propellant,
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Osnovy teorii i rascheta zhidkostnykh raketnykh dvigateley Kn. 2 - Fundamentals of the theory and calculation of liquid rocket engines - Book 2
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306:(today known as KhimMash). From 1960 onward, it powered several unmanned Soviet Spacecraft, including the first series of
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369:. Elastic barriers within the tank prevent the nitrogen gas and propellant/oxidiser from mixing with each other.
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The
Corrective Propulsion Unit consists of a single chamber 'S5.19' liquid rocket engine and a
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361:, igniting on contact. The rocket motor is supplied with fuel by pressurizing the tank using
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In 1974, it was replaced with its derived successor, the KDU-414A with the S5.114 engine.
31:
KDU-414 as seen on the "Russia in Space" exhibition (Airport
Frankfurt, Germany, 2002)
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443:"Spacecraft-propulsion blocks (KDU) from Isayev's design bureau (now Khimmash)"
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Russian
Planetary Exploration: History, Development, Legacy and Prospects
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The
Superpower Space Race: An Explosive Rivalry through the Solar System
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Soviet Robots in the Solar System: Mission
Technologies and Discoveries
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465:Основы теории и расчета жидкостных ракетных двигателей Кн. 2
581:. Springer Verlag, Praxis Publishing Ltd. p. 103.
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T. Huntress, JR., Wesley; Ya Marov, Mikhail (2011).
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293:Russian Корректирующая Двигательная Установка
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376:allows the engine to swivel along two axes.
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997:Rocket engines using the pressure-fed cycle
992:Rocket engines using hypergolic propellant
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560:: CS1 maint: location missing publisher (
467:. Moscow: Vysshaya Shkola. p. 20-21.
409:. Springer Verlag, Praxis Publishing Ltd.
25:
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18:
295:, Corrective Propulsion Unit), is a
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641:"Inventing The Interplanetary Probe"
629:from the original on 18 March 2022.
987:Rocket engines of the Soviet Union
651:from the original on 8 April 2022.
550:from the original on 11 July 2022.
449:from the original on 23 July 2021.
14:
260:Molniya satellites (First series)
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511:from the original on 2022-07-10.
497:. Springer Verlag. p. 195.
595:from the original on 2022-07-10
423:from the original on 2022-07-10
365:, which doubles as a source of
1:
708:Spacecraft engines and motors
460:V. M., Kudryavtseva (1993).
314:as well as the space probes
89:& Mid-course corrections
1002:Spacecraft attitude control
1018:
977:KB KhimMash rocket engines
880:
537:Космонавтика Энциклопедия
258:
24:
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531:Gluschko, V. P. (1985).
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892:Solid propellant motors
543:. Moscow. p. 159.
491:Reeves, Robert (2007).
403:Harvey, Brian (2007).
170:Thrust-to-weight ratio
936:Spacecraft propulsion
16:Type of rocket engine
956:Liquid apogee engine
674:at Wikimedia Commons
353:, and the oxidizer,
304:Isayev Design Bureau
185:1.18 MPa / 11.80 bar
77:Isayev Design Bureau
645:mentallandscape.com
217:Propellant capacity
162:445.5 lbf / 202 kgf
21:
308:Molniya satellites
103:Liquid-fuel engine
964:
963:
951:Apogee kick motor
670:Media related to
441:Brügge, Norbert.
312:Kosmos satellites
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264:Kosmos satellites
37:Country of origin
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363:gaseous nitrogen
241:2.42 ft / 0.74 m
233:3.34 ft / 1.02 m
191:Specific impulse
87:Attitude Control
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220:77 lb / 35 kg
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141:Configuration
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123:Mixture ratio
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67:Aleksei Isaev
65:
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597:. Retrieved
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425:. Retrieved
405:
378:
374:gimbal mount
371:
344:
297:pressure-fed
292:
288:
286:
135:Pressure-fed
73:Manufacturer
47:First flight
41:Soviet Union
715:Liquid fuel
154:Performance
83:Application
55:Last flight
971:Categories
941:Spacecraft
864:SuperDraco
599:2022-07-10
474:5060025632
427:2022-07-10
383:References
359:hypergolic
310:, several
225:Dimensions
109:Propellant
946:Satellite
921:SpaB-140C
619:"KDU-414"
556:cite book
201:Burn time
94:Successor
809:KTDU-425
649:Archived
627:Archived
593:Archived
545:Archived
509:Archived
447:Archived
421:Archived
320:Venera 1
272:Venera 1
246:Dry mass
238:Diameter
209:Restarts
193:, vacuum
181:pressure
179:Chamber
97:KDU-414A
63:Designer
918:SpaB-65
904:Star 48
899:Star 37
781:KTDU-80
762:KTDU-35
749:KDU-414
717:engines
672:KDU-414
347:conical
289:KDU-414
254:Used in
164:1.96 kN
146:Chamber
20:KDU-414
869:TR-201
802:S5.142
789:11D428
785:11D426
756:S5.114
585:
501:
471:
413:
332:KAUR-2
328:Zond 3
324:Zond 2
316:Mars 1
280:Zond 3
276:Zond 2
268:Mars 1
230:Length
914:FG-36
909:FG-15
874:XLR81
859:S5.92
844:RS-25
838:11D58
834:RD-58
814:LEROS
797:S5.80
793:S5.79
775:S5-66
772:S5-60
769:S5.53
766:S5-35
753:S5.19
744:Draco
739:Curie
724:17D61
548:(PDF)
541:(PDF)
355:IRFNA
196:272 s
131:Cycle
113:IRFNA
854:S5.4
849:S400
829:R-4D
824:LMDE
819:LMAE
734:BT-4
729:AJ10
583:ISBN
562:link
499:ISBN
469:ISBN
411:ISBN
351:UDMH
338:and
326:and
287:The
204:40 s
174:3.27
117:UDMH
58:1974
50:1960
340:3MV
336:2MV
126:2.6
973::
647:.
643:.
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621:.
608:^
591:.
558:}}
554:{{
517:^
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391:^
372:A
342:.
334:,
322:,
318:,
115:/
701:e
694:t
687:v
602:.
564:)
477:.
430:.
291:(
212:2
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