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
P4-1 Booster
P4-1
P4-1
Credit: Boeing / Rocketdyne
Rocketdyne LOx/Kerosene rocket engine. AQM-37. Target System Booster. Pressure-fed. First flight 1963.

AKA: LR64. Date: 1963. Thrust: 2.44 kN (549 lbf). Specific impulse: 232 s.

Propellant Formulation: IRFNA/Hydyne.



Country: USA. Propellants: Lox/Kerosene. 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