Encyclopedia Astronautica 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: 5 5 Crew Lifeboat - American manned rescue spacecraft. Study 1962. Five crew lifeboat capsule, separable, not re-entry capable, short duration. Mass per crew 284 kg. Status: Study 1962. Gross mass: 1,422 kg (3,134 lb). 5 inch HARP Gun - Canadian gun-launched sounding rocket. When most people think of the HARP Program they usually think of the big 16 inch guns roaring skywards as they launch test probes into the upper atmosphere. What most people do not realize was that even before HARP small portable gun launchers were used for the same purpose and even during HARP hundreds of high altitude flights were conducted using small guns. The 5 inch gun-launch system was initially designed to satisfy the requirements of the Meteorological Rocket Network This required that an 0.9 kg (2 lb) payload be carried to an altitude of 65 km (40 miles). Typical payloads were radar reflective chaff ejected at apogee, which was tracked by radar to yield wind data, and small Metsondes which drifted to earth under large parachutes and returned radio telemetry of temperature, humidity and the like. Status: Active. First Launch: 1965-02-02. Last Launch: 2008-04-10. Number: 124 . Payload: 10 kg (22 lb). 5 inch HARP Gun - Alternate designation for Gun Projectile 5-inch. 5 mlbf - Notional LOx/LH2 rocket engine. OOST, ROOST studies 1963. Status: Study 1963. Thrust: 41,361.00 kN (9,298,322 lbf). Propellants: Lox/LH2. 5 mlbf RP-4 - Notional LOx/Kerosene rocket engine. Study 1963. Operational date would have been July 1977. Recoverable stage. 10% plug nozzle. Used on Nova-1 DAC launch vehicle. Status: Study 1963. Thrust: 24,459.00 kN (5,498,601 lbf). Propellants: Lox/Kerosene. 5 Segment RSRM - Alternate name for RSRM. 5.5KS6100 - Alternate designation for Kiva 5.5KS6100 Solid rocket engine. 5.6KS5400 - Multiple-source American solid rocket engine. Nike Viper I second stage. Status: Retired 1960. Gross mass: 90 kg (198 lb). Unfuelled mass: 25 kg (55 lb). Thrust: 24.00 kN (5,395 lbf). Propellants: Solid. 5.9-KS-565 - Alternate designation for Star 6B Solid rocket engine. 500 lbf Centrojet - Manufacturer's designation of Centrojet Nitric acid-Amine rocket engine. 509th Research Institute - Fourth name of SISE. 50SAT - AKA Eagle-2, 50DollarSat; from Morehead State University. First PocketQube Cubesat; 1P size was 0.15 kg, 5 x 5 x 5cm cubes 51-KS-7,340 - Alternate designation for Star 30C Solid rocket engine. 51T6 - Russian anti-ballistic missile. Exo-atmospheric interceptor component of A-135 ABM system. Status: Active. First Launch: 1979-03-01. Last Launch: 2002-10-02. Number: 4 . Gross mass: 33,000 kg (72,000 lb). 51T6 Motor - Fakel solid rocket engine. A-925 first stage. Status: Active. Gross mass: 15,000 kg (33,000 lb). Unfuelled mass: 1,000 kg (2,200 lb). Propellants: Solid. 51T6 ZhRD engine series - 51T6, 53T6 - Article number for A-135. 51T6B ZhRD - Fakel N2O4/UDMH rocket engine. Propellants: N2O4/UDMH. 53T6 - Russian anti-ballistic missile. Endo-atmospheric interceptor component of A-135 ABM system. Status: Active. First Launch: 1979-08-01. Last Launch: 2014-05-08. Number: 12 . Gross mass: 10,000 kg (22,000 lb). Propellants: Solid. 54-KS-6,070 - Alternate designation for Star 30BP Solid rocket engine. 5500 - Article Number of KH-11 military surveillance satellite. 576F - Alternate name for Vandenberg OSTF1. 576G - Alternate name for Vandenberg OSTF2. 5D22 - SKB-350 solid rocket engine. A-350Zh second stage. Status: Retired 1967. Gross mass: 15,000 kg (33,000 lb). Unfuelled mass: 1,000 kg (2,200 lb). Propellants: Solid. 5D25 - Government designation of S5.44 Nitric acid-Amine rocket engine. 5K - Manufacturer's designation for Sever manned spacecraft. 5MV - Spacecraft bus developed by Lavochkin in the early 1980's for more ambitious planetary missions. 5MV - Manufacturer's designation for Taifun-1 military target satellite. 5NM - Manufacturer's designation for Mars 5NM mars lander. 5S47 - SKB-350 solid rocket engine. A-350Zh first stage. Status: Retired 1967. Gross mass: 15,000 kg (33,000 lb). Unfuelled mass: 1,000 kg (2,200 lb). Propellants: Solid. 5th Academy - First name of CAST. 5V11 - Article number for Dal. 5V21 - Article number for S-200. 5V28 - Article number for V-880. 5V28E - Article number for V-880E. 5V28M - Article number for V-880M. 5V55R - Article number for S-300. 5V55RM - Article number for S-300F. 5V55U - Article number for S-300PMU-1 5V55U. 5V91T - Article Number of IS-P military anti-satellite system target satellite. 5VK - Manufacturer's designation for Vega 5VK Venus probe. 5VS - Manufacturer's designation for Vega 5VS Venus probe. 5Ya24 - Article number for 218 missile. 5Ya24 - Article number for 218. 5Ya25 - Article number for 217 missile. 5Ya25 - Article number for 217. 5Ya25M - Article number for 217M. 5Ya26 - Article number for S-225. 5Ya26 - Article number for PRS-1 5Ya26. 5Ya26, 5Ya27 - Article number for S-225. 5Ya26, 5Ya27 - Article number for PRS-1 5Ya26. 5Ya27 - Alternate designation for S-225. 5Ya27 - Article number for PRS-1 5Ya26. 5Ya27 - Alternate name for V-825-1. 5Ya27 - Alternate name for V-825-0. 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