Accession Number:

AD0386386

Title:

APPLICATIONS STUDY FOR A HIGH-PERFORMANCE CRYOGENIC AEROSPIKE ROCKET ENGINE.

Descriptive Note:

Final rept. Mar 66-Oct 67 on Phase 1,

Corporate Author:

ROCKETDYNE CANOGA PARK CALIF

Personal Author(s):

Report Date:

1967-11-30

Pagination or Media Count:

409.0

Abstract:

This report presents application data for an advanced aerospike rocket engine utilizing LO2LH2 propellants. The engine concept was applied to six different stage configurations defined by the Air Force to represent the diversity of potential applications six vehicles were defined at 250K vacuum thrust level and six defined at a 350K level. A common engine module is defined for the six vehicle cases at each thrust level. Author

Subject Categories:

  • Liquid Propellant Rocket Engines
  • Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE