Accession Number:

AD0373137

Title:

Performance Characteristics of a Cryogenic Tripropellant System

Descriptive Note:

[Technical Report, Quarterly Report]

Corporate Author:

UNITED AIRCRAFT RESEARCH LABS EAST HARTFORD CT

Personal Author(s):

• Miller , Charles R.
• McFarlin , David J.
• Sadowski, Thomas J.

Report Date:

1966-06-01

Pagination or Media Count:

45

Abstract:

An investigation is being conducted to determine the performance characteristics of a cryogenic tripropellant system in small-scale thrust chambers. This report summarizes the work performed during the period March 1 through May 31, 1966.

Descriptors:

• air force
• rocket engines
• united states
• combustion
• combustion products
• test facilities
• contracts
• engineering
• military research
• combustion chambers
• exhaust gases
• jet propulsion
• physics laboratories
• propellant grains
• rockets
• solid propellants
• abstracts

Subject Categories:

• Rocket Propellants

Distribution Statement:

[A, Approved For Public Release]