Accession Number:
AD0423407
Title:
PRODUCT ENGINEERING PROGRAM. COATED METALLIC THRUST CHAMBERS EXPANDABLE NOZZLES COMBUSTION INSTABILITY SCALING CONCEPTS ABLATIVE THRUST CHAMBERS. WEAPON SYSTEM 107A-2
Descriptive Note:
Monthly progress rept. no. 4, 1-31 Oct 1963
Corporate Author:
AEROJET-GENERAL CORP SACRAMENTO CA
Personal Author(s):
Report Date:
1963-11-15
Pagination or Media Count:
32.0
Abstract:
Contents I. Coated Metallic Thrust Chambers II. Expandable Nozzles III. Combustion Instability Scaling Concepts IV. Ablative Thrust Chambers.
Descriptors:
Subject Categories:
- Liquid Propellant Rocket Engines