Accession Number:

AD0384855

Title:

ADVANCED AERODYNAMIC SPIKE CONFIGURATIONS. VOLUME 1. ANALYTICAL AND COLD FLOW STUDIES

Descriptive Note:

Final rept. 1 Jul 1964-28 Feb 1967

Corporate Author:

ROCKETDYNE CANOGA PARK CA

Personal Author(s):

Report Date:

1967-09-01

Pagination or Media Count:

471.0

Abstract:

Investigations of the aerodynamic spike nozzle concept are discussed in this report. Cold-flow test programs to evaluate high area ratio aerodynamic spike nozzles, engine segment testing techniques, and combustor configurations for aerodynamic spike nozzles were completed. A description of the models tested and the test results are presented. Analytical performance, weight, heat transfer, reliability and cost and design studies of the aerodynamic spike nozzle concept were conducted and the results are presented.

Subject Categories:

  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE