Accession Number:

ADA393835

Title:

Experimental Investigation of Hot-Gas Side Heat-Transfer Rates for a Hydrogen-Oxygen Rocket

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CENTER

Report Date:

1965-06-01

Pagination or Media Count:

25.0

Abstract:

An experimental investigation was conducted at the Lewis Research center to determine the hot-gas side heat-transfer rates in a rocket nozzle.

Subject Categories:

  • Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE