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:

• *LIQUID PROPELLANT ROCKET ENGINES
• *UNCONVENTIONAL NOZZLES
• ABLATION
• STABILITY
• PRODUCTION
• CORROSION
• THERMAL STRESSES
• NOZZLE INSERTS
• THERMAL INSULATION
• PERFORMANCE(ENGINEERING)
• COOLING
• COMBUSTION
• THERMAL CONDUCTIVITY

Subject Categories:

• Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE