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
P8E-9
P8E-9
P8E-9
Credit: Boeing / Rocketdyne
Rocketdyne Nitric acid/UDMH rocket engine. Lance Booster and Sustainer System. Pressure-fed. Sustainer 4400 -14,400 lbf, 227 sec Isp. Thrust and specific impulse values are at sea level. First flight 1972.

AKA: P8E. Date: 1964. Thrust: 205.44 kN (46,185 lbf). Specific impulse: 238 s. Specific impulse sea level: 238 s.

Thrust (sl): 205.440 kN (46,185 lbf). Thrust (sl): 20,950 kgf. Propellant Formulation: IRFNA/UDMH.



Family: Storable liquid. Country: USA. Propellants: Nitric acid/UDMH. Agency: Rocketdyne.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use