Accession Number : ADA259698


Title :   CPIA/M5 Liquid Propellant Engine Manual October 1992 Supplement (Unit No. 228)


Corporate Author : CHEMICAL PROPULSION INFORMATION AGENCY COLUMBIA MD


Report Date : Oct 1992


Pagination or Media Count : 8


Abstract : The HM-60 Vulcain engine is under development for Ariane 5 core stage application. It is a LO2LH2 gas generator cycle engine which develops a thrust of 1,075 kN (241,700 lb sub f) at vacuum conditions with a specific impulse of 4230 N*s/kg (431 lb sub f * sec/lbsub m).


Descriptors :   *LIQUID PROPELLANTS , *ROCKET ENGINES , FUELS , PROPULSION SYSTEMS , OXIDIZERS , MANUALS , LIQUID ROCKET OXIDIZERS , GAS GENERATOR ENGINES


Subject Categories : Information Science
      Liquid Propellant Rocket Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE