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
X4-AL-1000
Part of LR53 engine series Family
Aerojet Nitric acid/Amine rocket engine. Braking rocket for glider. Single uncooled chamber, pressure fed, 13 kg of propellant.

AKA: XLR9-AJ-1. Thrust: 4.41 kN (991 lbf). Burn time: 4.00 s. Height: 1.07 m (3.51 ft). Diameter: 0.36 m (1.18 ft).

Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 367 kg (809 lb). Chamber Pressure: 18.70 bar. Propellant Formulation: RFNA/Aniline.



Family: Storable liquid. Country: USA. Propellants: Nitric acid/Amine. Agency: Aerojet.

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