Mustard

home topic index

Engine Model: Mustard. Propellants: Lox/LH2. Thrust(vac): 2,157.400 kN (485,003 lbf). Thrust(sl): 1,598.100 kN (359,267 lbf). Isp: 405 sec. Isp (sea level): 300 sec. Burn time: 215 sec. Chambers: 1. Country: UK. Status: Study 1968. Mustard used on Rocket Stages Used on stage: Mustard. on launch vehicle: Mustard. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.