Accession Number:

ADA409847

Title:

Development Status of a 50k LOX/Hydrogen Upper Stage Demonstrator

Descriptive Note:

Conference paper

Corporate Author:

PRATT AND WHITNEY WEST PALM BEACH FL

Report Date:

2000-07-01

Pagination or Media Count:

12.0

Abstract:

This paper discusses design and systems integration status a 50,000 pound 222,4 kN thrust OxygenHydrogen Upper Stage Engine Demonstrator USD being created by Pratt Whitney Liquid Space Propulsion under contract for the United States Air Force Research Laboratory AFRL to support the Integrated High Payoff Rocket Propulsion Technology IHPRPT program. The objective of this program is to integrate advanced technology components into an expander cycle engine configuration and demonstrate a 1 increase in specific impulse, a 30 increase in engine thrust-to-weight, a 25 reduction in failures per 1000 uses, a 15 reduction in required support costs, and a 15 reduction in hardware costs relative to current state-of-the-art levels. Scheduled to be the first of the IHPRPT program engine demonstrators, test firing is planned in late 2001 to demonstrate a chamber pressure Pc capability of 1375 psia 9.48 Mpa. This integrated 50k LOXLH2 engine demonstrator will be used to evaluate individual component technologies as well as the system level mechanical, structural and thermodynamic interactions.

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE