Accession Number:

AD0373614

Title:

ADVANCED CRYOGENIC ROCKET ENGINE PROGRAM AEROSPIKE NOZZLE CONCEPT

Personal Author(s):

Corporate Author:

ROCKETDYNE CANOGA PARK CA CANOGA PARK United States

Report Date:

1966-06-30

Abstract:

Analysis and preliminary design of an advanced rocket engine using an aerospike nozzle and analysis, test hardware design, and test evaluation of thrust chamber performance and thrust chamber durability are described.

Descriptive Note:

Technical Report,01 Mar 1966,01 Jun 1966

Pages:

0128

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved For Public Release;

Contract Number:

AF 04(611)-11399

File Size:

8.01MB