Rocket engine
LR-87
Also known as LR-91
Rockets
Overview
The hypergolic (Aerozine 50 / N2O4) first- and second-stage engines (LR-87 / LR-91) of the Titan II, III, and IV families, valued for storable-propellant readiness on ICBM-derived launchers.
Components & hardware
Propellants
Powers
Knowledge connections
- PowersTitan II GLV
- PowersTitan IV
- Uses propellantAerozine 50 / N2O4
Sources
The primary and reference sources this topic draws on.
- Gunter's Space PageGunter Krebs — Gunter's Space Page
A specialist reference compilation of launch vehicles, stages, and spacecraft across all spacefaring nations.