Accession Number:

AD0368281

Title:

STORABLE TOROIDAL COMBUSTOR DEMONSTRATION PROGRAM.

Descriptive Note:

Quarterly progress rept. 1 Sep-30 Nov 65.

Corporate Author:

ROCKETDYNE CANOGA PARK CALIF

Personal Author(s):

Report Date:

1965-12-25

Pagination or Media Count:

56.0

Abstract:

Performance and cooling feasibility demonstrations are planned at 2000-psia chamber pressure with a 10,000-pound-thrust toroidal combustor using nitrogen tetroxide50 hydrazine-50 unsymmetrical dimethylhydrazine N2O4N2H4-UDMH, 50-50 propellants. Injectors, workhorse chambers, and cooled chambers are being designed and fabricated to support these demonstrations as discussed in this report. Results of a performance analysis are also presented. Author

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE