The Wayback Machine - https://web.archive.org/web/20161227193318/http://astronautix.com/l/lr87-11aj23-138.html
LR87-11 AJ23-138

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
LR87-11 AJ23-138
Part of LR87 Family
Aerojet N2O4/Aerozine-50 rocket engine. Version of LR-87-11 tuned for launch pad ignition when used on Titan 3B. First flight 1966.
See More

AKA: AJ23-138; LR87-11. Date: 1968. Thrust: 1,008.31 kN (226,677 lbf).

Thrust (sl): 1,008.310 kN (226,677 lbf). Thrust (sl): 102,820 kgf.

Family: Storable liquid. Country: USA. Launch Vehicles: Titan IIIB. Propellants: N2O4/Aerozine-50. 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