High Performance Divert and Attitude Control System (DACS) (TRW)

The TRW-built propulsion system for the Lockheed/Army Exoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS) provided both bipropellant divert thrust for vehicle steering and high- and low-level impulse for attitude control to enable the intercept of a high speed reentry vehicle in space.

Diverst and Attitude Control System Engine
Engine statistics
Specification
Propellants MON3 and MMH
O/F Ratio 1.6 to 1.8
Pc 1,500 psia
Cooling Method Ablative














Variable Thrust Engine : MRE-0.1