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List of unrealized projects of Soviet missile weapons

The following is a list of Soviet missile weapons projects , including those on which research, experimental and development work was carried out, which went through the stage of protecting the advance design and the project, bench and flight tests, and even were released by the factory method with limited experimental lots ( series) in order to conduct factory and state tests, but which for one reason or another have not been adopted.

Brief information about unrealized projects of Soviet missile weapons *
TitleType ofClassWork periodChief Designer (developer)Involved StructuresA brief description of the project, known tactical and technical and flight technical characteristics (maximum speed and flight altitude) and other information, the number of stages; target area parameters (range and altitude)Ex.AI
beginning of workcompletion of workhead officework contractors
10-xSSW — W1945Chelomei V.N.OKB-51 NKAP → MAPcontrol system - electric autopilot AP-4> 70[1] [2] [3] [4] [5] [6]
OKB Ch. designer I.V. Chetverikov at plant No. 458 NKAP , factory No. 51 NKAP , factory No. 456 NKAP → MAP , OKB-3 MAP
10-XHSSW — W1945Chelomei V.N.OKB-51 MAP → Branch OKB-155 MAPfrom the German Fau-1 and its predecessor 10-X, the subsequent products were distinguished by a greater range and speed of flight, accuracy of hit. Tu-2 , Tu-4 , Pe-8 were provided as carrier aircraft; power plant - PuVRD[7] [5]
11-xSSW — W1944Chelomei V.N.OKB-51 NKAPdraft design prepared; power plant - PuVRDn / a[8]
12-xSSW — W1944Chelomei V.N.OKB-51 NKAPdraft design prepared; power plant - PuVRDn / a[8]
14-XSSW — W1945Chelomei V.N.OKB-51 MAPpower plant - PuVRD D-5[7]
16-X SurfSSW — W1945Chelomei V.N. → Alekseev S.M.OKB-51 MAP → OPZ-1 → SZ-1 MAP → Branch OKB-155 MAPOKB-3 MAPpower plant - 2 × mid-flight PuVRD D14-4a, carrier aircraft - Tu-4, maximum speed - over 900 km / hn / a[9] [4] [5] [10]
A-300BRZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - three- or four-stage; 1st stage - 10 × NK-9 LRE on kerosene / oxygen, 2nd and 3rd stages - hydrogen / oxygen LRE , starting weight - 300 t, payload - 8 t-[eleven]
A-300-1BRZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - three- or four-stage; 1st stage - LRE on kerosene / oxygen, 2nd and 3rd stages - LRE on hydrogen / oxygen, starting weight - 300 t-[12]
A-300-2BRZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - three- or four-stage; 1st stage - LRE on kerosene / oxygen, 2nd and 3rd stages - LRE on hydrogen / oxygen, starting weight - 300 t-[12]
A-1750BRZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - three- or four-stage; 1st stage - LRE on kerosene / oxygen, 2nd and 3rd stages - LRE on hydrogen / oxygen, payload - 85 t-[13]
A-2000BRZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - three- or four-stage; 1st stage - LRE on kerosene / oxygen, 2nd and 3rd stages - LRE on hydrogen / oxygen, starting weight - 1950 t, payload - 85 t-[13]
StormKRW — BLavochkin S. A.OKB-301 MAPn / a
"Wave"SSM — ZChelomei V.N.OKB-51 MAPpower plant - PuVRD? ; submarine shell[fourteen]
GR-1BRZ — Z1968Korolev S.P.OKB-1 MOSmovable on a tracked chassis; power plant - three-stage liquid fuel, starting weight - 200 tons, length - 39 m, diameter - 2.75 m, firing range - 12000 km, guidance system - ANNn / a[fifteen]
ZUR-215UrW — B19591959one
SAM-400UrW — Bguidance system - ARLGS "Zenit-2"n / a[16]
ZURDDKRW — B19591959Chelomei V.N.OKB-52 GKATpower plant - two-stage-[17]
ZURDD-400KRW — B19591959Chelomei V.N.OKB-52 GKATpower plant - two-stage: 1 × starting solid propellant rocket propulsion system , 1 × mid- flight engine ; launch weight - 6800 kg, cruising speed - 3708 km / h, range of the affected area - 400 km, interception height - 35 km-[eighteen]
ZURDD-600KRW — B19591959Chelomei V.N.OKB-52 GKATpower plant - two-stage; launch weight - 9 tons, range of the affected area - 600 km-[19]
ZURDD-BKRW — B19591959Chelomei V.N.OKB-52 GKATrocket with a vertical launch, the power plant - two-stage; Marching speed - 4939 km / h, maximum speed - 9261 km / h, flight altitude - 60 km, interception altitude - 40 km; design plan: the rocket at maximum speed was brought to a stationary height, and then planned in order to achieve the target at marching speed with minimal energy consumption at the height of interception (planning with periodic turning on of the marching engine - “ Zenger ” planning)-[19]
K-35UrB – B1958Yakovlev A.S.OKB-145 GKATarmament of fighter-interceptor Yak-35MVn / a
K-9-51UrB – B1958Sukhoi P.O.OKB-51 GKATarmament of fighter interceptors T-37n / a
K-9-155UrB – B1958Mikoyan A.I.OKB-155 GKATarmament of fighter interceptors E-150n / a
CBDCBDZ — Z19591959Chelomei V.N.OKB-52 GKATpower plant - four-stage; 1st stage weight - 107 t-[19]
CBDCBDZ — Z19591960Chelomei V.N.OKB-52 GKATpower plant - solid propellant rocket engine-[twenty]
CBD-12000CBDZ — Z19591959Chelomei V.N.OKB-52 GKATpower plant - three-stage; 1st stage mass - 85 t, top speed - 22,680 km / h, flight range - 12,000 km-[19]
The copSSW — W1955Bereznyak A.Ya.OKB-256 (as part of OKB-155 ) MAPair-based projectile for arming missile aircraftn / a[21]
KSSSSM — Z1955Bereznyak A.Ya.OKB-256 (as part of OKB-155 ) MAPsea-based projectile for armament of surface shipsn / a[21] [14]
P-10SSM — Z19551957Beriev G.M.OKB-49 MAP , TsKB-18 GKSsurface launch shell for submarines; two-stage power plant: 1st stage - solid fuel (powder rocket engines), 2nd march stage - turbojet engine, flight height - up to 1200 m, practical ceiling - 400 m16[22] [23]
TsAGI , LII MAP , NII-303 , TsKB-18 , OKB-155 , Design Bureau of Plant No. 81 MAP , a serial plant named after G. Dimitrova MAP, Plant No. 402 GKS , 28th Research Institute of the Navy
P-100SSM — Z1957Beriev G.M.OKB-49 MAPlong-range supersonic surface launch shell for submarines; developed simultaneously with the R-11FM ballistic missile, which at that time was undergoing flight tests; power plant - ramjetn / a[21] [24]
P-20SSM — Z1955Ilyushin S.V.OKB-240 MAP → GKAT → MAPsupersonic guidance system - guidance station AR-12n / a[21] [14] [25]
R-15BRM — Z1960sYangel M.K.OKB-586 MOSSLBMn / a[26]
R-3BRZ — ZKorolev S.P.OKB-1 MOSground based; power plant - single-stage on liquid fuel, starting weight - 72 t, length - 27 m, diameter - 2.8 m, firing range - 3000 km, guidance system - ANNn / a[27]
RZ-25 / 5V11 "Dal"UrW — BLavochkin S. A.OKB-301 MAP → GKATn / a
RM-500KRW — B19581961Mikoyan A.I.OKB-155 GKATKB-1power plant - two-stage; starting mass - 7–8 tons, cruising speed - 4700 km / h, range of interception - 800–1000 km, height of interception - 25–35 kmn / a[twenty]
RCCUrW — WTsybin P.V.OKB-1 MOSOKB-256 GKATdesign plan - launch from Tu-95N or A-57 carrier aircraftn / a[28] [29]
RT-15MBRM — Z1963SLBM underwater launch; the power plant is a two-stage solid fuel, length - 10.5 m, diameter - 1.5 m, firing range - 2400 km, guidance system - ANNn / a[thirty]
RF-500KRW — B19591960Chelomei V.N.OKB-52 GKATKB-1power plant - two-stage; starting weight - 7–8 tons, cruising speed - 3500 km / h, range of interception - 500–600 km, height of interception - 35–40 km-[31]
UKBR (UB)CBDZ — Z19601960Chelomei V.N.OKB-52 GKATpower plant - solid propellant rocket engine-[32]
n / aBRZ — Z19601960Chelomei V.N.OKB-52 GKATlaunch weight - 150 tons, warhead - winged warhead with homing in the final flight section or a controlled satellite for targeting cruise missiles-[twenty]
n / aBRZ — Z19601960Chelomei V.N.OKB-52 GKATlaunch weight - 1,500 tons, warhead - winged warhead with homing at the end of the flight-[twenty]
n / aCBDP — P19601960Chelomei V.N.OKB-52 GKATmissile for hitting surface and ground targets, warhead - with homingn / a[33]
* In the presented classification of missiles, the wordings “land” and “surface” are not synonyms, since the second assumes: 1) In relation to the basing environment - the presence of both land and sea versions of basing a specific type of missile weapon (or the possibility of such basing if the project did not go beyond the scope of research work); 2) With regard to targets - the multipurpose nature of missiles that are equally suitable for hitting both land and sea targets.
The list uses the terms “aircraft-projectile” and “cruise missile” according to the nomenclature of missile and artillery weapons of that time (chronologically, the term “aircraft-projectile” was used until 1960, after which it was replaced by the phrase “cruise missile”).

See also

  • List of unrealized projects of Soviet military aviation
  • List of early US Army and Air Force missile projects

Notes

  1. ↑ Polyachenko V.A. At sea and in space, 2008 , p. nineteen.
  2. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 1, p. 452.
  3. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 1, p. 464.
  4. ↑ 1 2 Tikhonov S. G. Defense enterprises of the USSR and Russia, 2010 , T. 1, p. 492.
  5. ↑ 1 2 3 Tikhonov S. G. Defense enterprises of the USSR and Russia, 2010 , T. 1, p. 508.
  6. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 2, p. 268–269.
  7. ↑ 1 2 Polyachenko V.A. At sea and in space, 2008 , p. twenty.
  8. ↑ 1 2 Evteev I. M. The flame still rose, 1997 , p. 23.
  9. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 20-21.
  10. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 2, p. 273.
  11. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 63–67.
  12. ↑ 1 2 Polyachenko V.A. At sea and in space, 2008 , p. 63.
  13. ↑ 1 2 Polyachenko V.A. At sea and in space, 2008 , p. 63–64.
  14. ↑ 1 2 3 Polyachenko V.A. At sea and in space, 2008 , p. 47.
  15. ↑ Karpenko A.V. Russian missile weapons, 1993 , p. 10, 12.
  16. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 2, p. 118.
  17. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 52.
  18. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 52–53.
  19. ↑ 1 2 3 4 Polyachenko V.A. At sea and in space, 2008 , p. 53.
  20. ↑ 1 2 3 4 Polyachenko V.A. At sea and in space, 2008 , p. 59.
  21. ↑ 1 2 3 4 Polyachenko V.A. At sea and in space, 2008 , p. 35.
  22. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 34–37.
  23. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 39–47.
  24. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 47–48.
  25. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 2, p. 71.
  26. ↑ Karpenko A.V. Russian missile weapons, 1993 , p. 28.
  27. ↑ Karpenko A.V. Russian missile weapons, 1993 , p. eleven.
  28. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 74.
  29. ↑ Tikhonov S.G. Defense enterprises of the USSR and Russia, 2010 , vol. 2, p. 93.
  30. ↑ Karpenko A.V. Russian missile weapons, 1993 , p. 28–29.
  31. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 54-60.
  32. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 68.
  33. ↑ Polyachenko V.A. At sea and in space, 2008 , p. 67.

Literature

  • Evteev I. M. The flame was still rising ... Essays. - M .: Inter-Libra, 1997 .-- 264 p. - Circulation of 1 thousand copies. - ISBN 5-86490-060-5 .
  • Karpenko A. V. Russian missile weapons 1943–1993 Directory. - 2nd ed., Rev. and add. - St. Petersburg: Pika, 1993 .-- 180 s. - Circulation of 1 thousand copies.
  • Pervushin A.I. Battle for the stars: space confrontation. - M .: AST , 2004 .-- 831 s. - (Military Historical Library) - ISBN 5-17-024200-X .
  • Polyachenko V. A. At sea and in space: Memoirs. - St. Petersburg: Morsar AB, 2008 .-- 224 p. - Circulation 1500 copies. - ISBN 5-93599-001-8 .
  • Tikhonov S.G.
Defense enterprises of the USSR and Russia: in 2 volumes. - M .: TOM, 2010 .-- T.1 - 608 p. - Circulation of 1 thousand copies. - ISBN 978-5-903603-02-2 .
Defense enterprises of the USSR and Russia: in 2 volumes. - M .: TOM, 2010 .-- T.2 - 608 p. - Circulation of 1 thousand copies. - ISBN 978-5-903603-03-9 .
  Unrealized Soviet projects
Military and civil aviation • Armored vehicles • Hydronics • Cosmonautics • Industry and Agriculture • Fuel and energy complex and Nuclear power • Rocket building • Transport • Navy • Economy • Electronics
Source - https://ru.wikipedia.org/w/index.php?title=List of unrealized_projects of Soviet_ missile_arms&oldid = 95771170


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