The Wayback Machine - https://web.archive.org/web/20161228042034/http://astronautix.com/x/xlr53aj-1.html
XLR53AJ-1

Encyclopedia Astronautica
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
XLR53AJ-1
Part of LR53 engine series Family
Aerojet Nitric acid/Amine rocket engine. Development begun 1949. Superperformance, wing tip mounted, regenerative cooling, pressure fed, 240 sec duration, 1000 lbf thrust each.
See More

AKA: XLR53-AJ-1. Status: Out of Production. Date: 1949. Thrust: 4.41 kN (991 lbf).

Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.

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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use