Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Encyclopedia Astronautica Index: 8 87.2-KS-17,335 - Alternate designation for Star 48A s. 87.2-KS-17,335 - Alternate designation for Star 48B s and [Star 48B s] solid rocket engines. 87.2-KS-17,735 - Alternate designation for Star 48B Solid rocket engine. 8A11 - Article number for R-1 stage. 8A11 - Article number for R-1. 8A61 - Article number for R-11 stage. 8A61 - Article number for R-11. 8A62 - Article number for R-5 rocket stage. 8A62M - Article number for R-5M. 8A63 - Article number for R-3A. 8A67 - Article number for R-3. 8A91 - Article number for Sputnik 8A91. 8A92 - Article number for Vostok 8A92. 8A92M - Article number for Vostok 8A92M. 8D21 - Article Number of RD-301 LF2-Ammonia rocket engine. 8D411K - Article Number of RD-0210 N2O4-UDMH rocket engine. 8D412K - Article Number of RD-0211 N2O4-UDMH rocket engine. 8D415K - Kosberg LOx/Kerosene rocket engine. Designed for use in N-1. Development canceled in 1960 when Korolev turned to Kuznetsov for R-9 and N-1 engines after continuous rows with Glushko over performance and propellant types. First flight was planned for 1966. Status: Developed 1960-. Date: 1960-. Thrust: 1,471.00 kN (330,693 lbf). Propellants: Lox/Kerosene. 8D419 - Manufacturer's designation of 8D423 N2O4-UDMH rocket engine. 8D420 - Article Number of RD-270 N2O4-UDMH rocket engine. 8D420M - Article Number of RD-270M N2O4-Pentaborane rocket engine. 8D423 - Izotov N2O4/UDMH rocket engine. Production from 1964. Single chamber engine for UR-100 stage 2. Gas generator cycle with two large turbine exhaust pipes. First flight 1965. Later modified for the LK-700 manned lunar landeer. Status: Design 1964. Number: 282 . Thrust: 131.00 kN (29,449 lbf). Propellants: N2O4/UDMH. 8D43 - Kosberg N2O4/UDMH rocket engine. UR-500 stage 1 original concept. Hardware. In early Proton design would be clustered with 4 x Glushko 11D43. Abandoned in favor of 6 x Glushko 11D48, but later developed into the RD-0208 and RD-0210. Status: Hardware. Thrust: 559.00 kN (125,668 lbf). Propellants: N2O4/UDMH. 8D43 + 11D43 - Kosberg N2O4/UDMH rocket engine. Design 1962. Originally the first stage of the Proton was designed for 4 x fixed 11D43 and 4 x gimbaled Kosberg 8D43; replaced by 6 x 11D48 from Glushko in final Proton design. Status: Design 1962. Thrust: 2,247.45 kN (505,247 lbf). Propellants: N2O4/UDMH. 8D44 - Article Number of RD-0203 N2O4-UDMH rocket engine. 8D45 - Article Number of RD-0202 N2O4-UDMH rocket engine. 8D46 - Article Number of RD-0205 N2O4-UDMH rocket engine. 8D47 - Article Number of RD-0206 N2O4-UDMH rocket engine. 8D48 - Article Number of RD-0213 N2O4-UDMH rocket engine. 8D49 - Article number for RD-0210. 8D49 - Article Number of RD-0212 N2O4-UDMH rocket engine. 8D515 - Article Number of RD-217 Nitric acid-UDMH rocket engine. 8D52 - Article Number of RD-103 LOx-Alcohol rocket engine. 8D52M - Article Number of RD-103M LOx-Alcohol rocket engine. 8D63 - Article Number of RD-851 Nitric acid-UDMH rocket engine. 8D67 - Article Number of RD-0207 N2O4-UDMH rocket engine. 8D71 - Article number for RD-105. 8D71 - Article Number of RD-103 LOx-Alcohol rocket engine and [RD-103] LOx-Kerosene rocket engine. 8D710 - Article Number of RD-119 LOx-UDMH rocket engine. 8D711 - Article Number of RD-109 LOx-UDMH rocket engine. 8D712 - Article Number of RD-218 Nitric acid-UDMH rocket engine. 8D713 - Article Number of RD-219 Nitric acid-UDMH rocket engine. 8D714 - Article Number of RD-0105 LOx-Kerosene rocket engine. 8D715 - Article Number of RD-0106 LOx-Kerosene rocket engine. 8D715K - Article number for RD-0108. 8D715K - Article Number of RD-0107 LOx-Kerosene rocket engine. 8D715P - Article Number of RD-0108 LOx-Kerosene rocket engine. 8D716 - Article Number of RD-111 LOx-Kerosene rocket engine. 8D719 - Article Number of RD-0109 LOx-Kerosene rocket engine. 8D72? - Article Number of RD-106 LOx-Kerosene rocket engine. 8D721 - Article Number of RD-224 Nitric acid-UDMH rocket engine. 8D723 - Article number for RD-250. 8D723 - Article Number of RD-251 and [RD-251] N2O4-UDMH rocket engines. 8D725 - Glushko N2O4/UDMH rocket engine. Developed 1963-1970. 10 to 12 metric ton thrust engine developed for an unstated military requirement. Status: Developed 1963-1970. Date: 1963-1970. Thrust: 117.00 kN (26,302 lbf). Propellants: N2O4/UDMH. 8D726 - Korolev LOx/Kerosene rocket engine. GR-1 Stage 3, N-11GR - V. Development based on S1.5400. Thrust: 66.70 kN (14,995 lbf). Propellants: Lox/Kerosene. 8D727 - Article Number of RD-108-8D727 LOx-Kerosene rocket engine. 8D727K - Article number for RD-108-8D727. 8D727K - Article Number of RD-108-8D727K LOx-Kerosene rocket engine. 8D727K, 8D727P - Article Number for RD-108-8D727 LOx-Kerosene rocket engine. 8D727P - Alternate name for RD-108-8D727. 8D728 - Article Number of RD-107-8D728 LOx-Kerosene rocket engine. 8D74 - Article Number of RD-107-8D74 LOx-Kerosene rocket engine. 8D74-1958 - Article Number of RD-107-8D74-1958 LOx-Kerosene rocket engine. 8D74-1959 - Article Number of RD-107-8D74-1959 LOx-Kerosene rocket engine. 8D74K - Article Number of RD-107-8D74K LOx-Kerosene rocket engine. 8D74PS - Article Number of RD-107-8D74PS LOx-Kerosene rocket engine. 8D75 - Article Number of RD-108-8D75 LOx-Kerosene rocket engine. 8D75-1958 - Article Number of RD-108-8D75-1958 LOx-Kerosene rocket engine. 8D75-1959 - Article Number of RD-108-8D75-1959 LOx-Kerosene rocket engine. 8D75K - Article Number of RD-108-8D75K LOx-Kerosene rocket engine. 8D75PS - Article Number of RD-108-8D75PS LOx-Kerosene rocket engine. 8D76 - Article Number of RD-107-8D76 LOx-Kerosene rocket engine. 8D77 - Article Number of RD-108-8D77 LOx-Kerosene rocket engine. 8D811 - Article Number of RD-0214 N2O4-UDMH rocket engine. 8EK - Article Number of Luna Ye-8 lunar rover. 8F021 - Article Number of OGCh military orbital bombing system. 8F17 - Article number for R-16. 8K - Manufacturer's designation for Zenit-8 military surveillance satellite. 8K11 - Article number for R-1. 8K14 - Article number for R-11. 8K14 - Article number for R-11A. 8K14 - Article number for R-17 stage. 8K14 - Article number for R-11M. 8K14, SS-1C Scud B, 9K72 Elbrus - Article number for R-17 stage rocket stage. 8K51 - Article number for R-5M. 8K513 - Russian anti-satellite missile. ASAT version. Little has emerged about Korolev's ASAT project, designed in competition with Chelomei's in 1961-1964. Payload: 1,500 kg (3,300 lb). 8K513 Blok A - Article number for GR-1 Stage 1 rocket stage. 8K513 Blok B - LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle mass of 117 metric tons. Developed into Molniya/Soyuz second stage. Gross mass: 25,000 kg (55,000 lb). Unfuelled mass: 2,100 kg (4,600 lb). Thrust: 441.00 kN (99,140 lbf). Propellants: Lox/Kerosene. 8K513 Blok V - Article number for GR-1 Stage 3 rocket stage. 8K61 - Article number for R-11FM. 8K62 - Article number for R-5. 8K63 - Article number for R-12. 8K63U - Article number for R-12U. 8K64 - Article number for R-16. 8K64U - Article number for R-16U. 8K65 - Article numbe for R-14. 8K65U - Article number for R-14U. 8K66 - Article number for R-26-1. 8K66 - Article number for R-26-2. 8K66 - Article number for R-26. 8K67 - Article number for Tsiklon. 8K67P - Article number for R-36 8K67P. 8K68 - Article number for R-56 Polyblock ICBM. 8K68 - Article number for R-56. 8K68 - Article number for R-56 Polyblock. 8K69 - Article number for R-36O 8K69. 8K69 - Article number for R-36-O. 8K71 - Article number for R-7. 8K711 - Russian ballistic missile. Korolev project. No other information available. Status: Study 1961. 8K713 - Article Number of intercontinental ballistic missile version of the GR-1 global rocket. Article number sometimes erroneously given as 8K73. 8K713 - Article number for GR-1. 8K71PS - Article number for Sputnik 8K71PS. 8K72 - Article number for Vostok 8K72. 8K72 - Article number for Vostok-L 8K72. 8K72 - Article number for Luna 8K72. 8K72K - Article number for Vostok 8K72K. 8K72K - Article number for Vostok 8A92. 8K73 - Russian ballistic missile. Korolev project. Probably designation for intercontinental ballistic missile variant of his GR-1 global rocket. Status: Study. 8K73 - Article number for 8K713. 8K74 - Article number for Molniya 8K78. 8K74 - Article number for R-7A. 8K75 - Article number for Desna. 8K75 - Article number for R-9A. 8K75 - Article number for Romashka. 8K75 - Article number for Dolina. 8K75M - Article number for R-9M. 8K76 - Russian intercontinental ballistic missile. Version using storable propellants and Isayev engines. Studied but rejected prior to start of development. 8K76 - Article number for R-9M. 8K77 - Russian intercontinental ballistic missile. Version with vacuum-isolated liquid oxygen tanks to provide capability to hold ready for instant launch. Studied but never developed. 8K77 Blok A - Article number for R-9A Stage 1 rocket stage. 8K77 Blok B - Article number for R-9A Stage 2 rocket stage. 8K78 - Article number for Molniya 8K78. 8K78L - Article number for Molniya 8K78L. 8K78M - Article number for Molniya 8K78M. 8K79 - Russian intermediate range ballistic missile. Korolev 1961 design for a single stage military rocket. A competing missile was selected for the requirement. Status: Study 1960. Gross mass: 25,000 kg (55,000 lb). Payload: 800 kg (1,760 lb). 8K81 - Article number for UR-200. 8K81 Stage 1 - Article number for UR-200-1 rocket stage. 8K81 Stage 2 - Article number for UR-200-2 rocket stage. 8K82 - Article number for UR-500. 8K82K - Article number for Proton-K. 8K82K - Article number for Proton K. 8K82K / 11S824 - Article number for Proton-K/D. 8K82K / 11S824 - Article number for Proton K/D. 8K82K / 11S824F - Article number for Proton-K/D-2. 8K82K / 11S824F - Article number for Proton K/D-2. 8K82K / 11S824M - Article number for Proton-K/D-1. 8K82K / 11S824M - Article number for Proton K/D-1. 8K82K / 11S86 - Article number for Proton-K/DM. 8K82K / 11S86 - Article number for Proton K/DM. 8K82K / 11S861 - Article number for Proton-K/DM-2. 8K82K / 11S861 - Article number for Proton K/DM-2. 8K82K / 11S861-01 - Article number for Proton-K/DM-2M. 8K82K / 11S861-01 - Article number for Proton K/DM-2M. 8K82K / 17S40 - Article number for Proton-K/17S40. 8K82K / 17S40 - Article number for Proton K/17S40. 8K82KM - Article number for Proton/Briz K/M. 8K82KM - Article number for Proton KM-4 Briz M. 8K82M - Article number for Proton-M/Briz-M. 8K82M / 11S861 - Article number for Proton-M/DM-2. 8K83 - Article number for UR-200B. 8K84 - Article number for Taran. 8K84 - Article number for UR-100. 8K84 Stage 1 - Article number for 8S816 rocket stage. 8K84 Stage 2 - Article number for 8S817 rocket stage. 8K84K - Article number for UR-100K. 8K84M - Article number for UR-100M. 8K84UTTKh - Article number for UR-100M. 8K94 - Article number for 8K94 stage. 8K94 - Ukrainian intermediate range ballistic missile. Unusual designation for the upper stages of another Yangel project - possibly reflecting design originally was stand-alone IRBM? Status: Design 1962. 8K94 stage - N2O4/UDMH propellant rocket stage. Unusual designation for the upper stage of another Yangel project - possibly reflecting that the design originally was a stand-alone IRBM? Empty mass estimated. Status: Retired 1969. Gross mass: 9,800 kg (21,600 lb). Unfuelled mass: 900 kg (1,980 lb). Thrust: 147.00 kN (33,046 lbf). Propellants: N2O4/UDMH. 8K95 - Article number for RT-1. 8K96 - Article number for RT-15. 8K97 - Article number for RT-25. 8K98 - Article number for RT-2. 8K98M - Article number for RT-2M. 8K98P - Article number for RT-2P. 8K99 - Article number for RT-20P. 8K99 - Article number for RT-20. 8S810K - Article number for Proton K-1 rocket stage. 8S811K - Article number for Proton K-2 rocket stage. 8S816 - N2O4/UDMH propellant rocket stage. Orevo has sectioned hardware. Total mass, sea level thrust accurate; Isp, empty mass and burn time estimated. Source: Placard, Orevo. Status: Retired 1984. Gross mass: 32,799 kg (72,309 lb). Unfuelled mass: 3,000 kg (6,600 lb). Thrust: 868.80 kN (195,314 lbf). Propellants: N2O4/UDMH. 8S817 - N2O4/UDMH propellant rocket stage. Orevo has sectioned hardware. Total mass, thrust accurate; Isp, empty mass and burn time estimated. Source: Placard, Orevo. Status: Retired 1984. Gross mass: 8,611 kg (18,984 lb). Unfuelled mass: 900 kg (1,980 lb). Thrust: 131.45 kN (29,551 lbf). Propellants: N2O4/UDMH. 8th Academy - First name of SAST. 8Zh38 - Article number for R-2 stage. 8Zh38 - Article number for R-2. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z � 1997-2016 Mark Wade - Contact � / Conditions for Use |
