Accession Number:

AD0750591

Title:

Comparison of Performance of a Double-Cornered Plug Nozzle with a Conventional Convergent-Divergent Rocket Nozzle

Descriptive Note:

Technical rept.

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL PROPULSION DIRECTORATE

Personal Author(s):

Report Date:

1972-06-30

Pagination or Media Count:

46.0

Abstract:

The report presents performance data for double-cornered plug nozzles for comparison with convergent-divergent nozzles. A conventional convergent- divergent C-D nozzle was used to develop the propellant charge, ignition and ballistics, and as a baseline for plug nozzle performance evaluation. Author

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE