Accession Number:

AD0368603

Title:

MANEUVERING SATELLITE PROPULSION SYSTEM DEMONSTRATION. PART 3

Descriptive Note:

Final rept. May 1964-Jul 1965

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO NY

Personal Author(s):

Report Date:

1965-12-01

Pagination or Media Count:

248.0

Abstract:

This document presents the exploratory development work accomplished in the design, fabrication and testing of advanced rocket engine components for a high-energy-propellant, space maneuvering vehicle. The exploratory development effort consisted of a series of critical experiments to determine operational capabilities of high temperature material and coating in fluorine rich and HF environments, the feasibility of a wide range throttling concept utilizing mixed phase propellants, and the feasibility of an advanced thrust chamber cooling concept.

Subject Categories:

  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE