Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 26-Jun-2019

INTERORBITAL SYSTEMS (IOS)

(USA)


INTERORBITAL SYSTEMS (IOS) engine specifications

Manufacturer of liquid-fuel engines for rockets, satellites, boosters and vernier thrusters.

GPRE 6-0 KNHx running
“GPRE 6-0 KNHx running”

Main models: GPRE stands for "General Purpose Rocket Engine". They have ablative cooling.

-GPRE 0.5KNF, 500 lbf of thrust. (Nitric Acid / Furfuryl Alcohol).

-GPRE 0.5KNHx, 500 lbf of thrust. (Nitric Acid / Hydrocarbon X).

-GPRE 2.5 KLM, 2,500 lbf of thrust. (Liquid oxygen / Methanol)..

-GPRE 6.0 KNHx, 6,000 lbf of thrust. (Nitric Acid / Hydrocarbon X).

Engines of INTERORBITAL SYSTEMS (IOS)

Model: GPRE 0.5 KNF

Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 500 Lbf
Weight:

Other details:
Model: GPRE 0.5 KNHx

Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 500 Lbf
Weight:

Other details:
Model: GPRE 2.5 KLM

Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 2500 Lbf
Weight:

Other details:
Model: GPRE 6.0 KNHx

Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 6000 Lbf
Weight:

Other details: