Accession Number:

AD0504212

Title:

Advanced Maneuvering Propulsion Technology Program

Corporate Author:

ROCKETDYNE CANOGA PARK CA

Report Date:

1969-09-01

Abstract:

The engine design and analysis task was continued with a 1 detailed parametric analysis of thrust chamber temperature and pressure drop characteristics, 2 revision of the engine balance, and 3 continued main oxidizer and turbine control valve design activity. The engine critical component task effort was primarily directed toward the completion of fabrication of the prototype channel-wall thrust chamber segment. Design of the main thrust chamber nozzle has been completed and design of the base closure and secondary engine nozzle simulator is nearing completion.

Descriptive Note:

Quarterly progress rept. no. 7, 1 May-31 Jul 1969

Supplementary Note:

Pages:

0182

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

Contract Number:

F04611-67-C-0116

Contract Number 2: