RS-27A Engine

The nominal 200,000 lb. sea-level thrust RS-27A powers the Delta II launch vehicle and has compiled one of the most consistent and successful launch records in the history of rocketry with a 100-percent reliability factor.

A single-start power plant is gimbal-mounted and operates on a combination of liquid oxygen and RP-1 (kerosene). The thrust chamber is regeneratively cooled with fuel circulating through tubes that comprise the thrust chamber.

The RS-27A is the latest version of this propulsion system that includes a higher 12:1 area expansion ratio thrust chamber nozzle among other improvements. The RS-27A is used as the main booster propulsion system for the Delta II family of launch vehicles.

Specifications

Propellants

Thrust

Specific Impulse

Dimensions

Fuel: RP-1
Oxidizer: Liquid Oxygen

 

Vacuum: 237,000 lb.
Sea Level: 200,000 lb.

Vacuum: 302 sec.
Sea Level: 255 sec.
Area Ratio: 12:1
Chamber Pressure: 700 psia
Engine Mixture Ratio: 2.2 

Length: 149 in.
Diameter: 67 in.
Weight: 2,530 lb.