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RS-19


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RS-19
Credit: Boeing / Rocketdyne Rocketdyne exotic ClF3/Hydrazine rocket engine. Condor Development Booster Air-to-Ground Missile. Pressure-fed. Thrust and specific impulse values are at sea level.

Date: 1967. Thrust: 3.11 kN (699 lbf). Specific impulse: 259 s. Specific impulse sea level: 259 s.

Thrust (sl): 3.108 kN (699 lbf). Thrust (sl): 317 kgf. Propellant Formulation: ClF3/MHF-3.

Family: Exotic. Country: USA. Launch Vehicles: Condor. Propellants: ClF3/Hydrazine. Agency: Rocketdyne. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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