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
RS-19
RS-19
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.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use