Accession Number:

AD0839278

Title:

FLEXIBLE EXIT CONE NOZZLE DEVELOPMENT PROGRAM. VOLUME II. COLD FLOW TESTS DATA (PLOTTED). APPENDIX I

Descriptive Note:

Final rept. 15 Mar 1967-31 Jul 1968 on Phase 2

Corporate Author:

MORTON THIOKOL INC BRIGHAM CITY UT WASATCH OPERATIONS

Personal Author(s):

Report Date:

1968-08-01

Pagination or Media Count:

151.0

Abstract:

Descriptors:

• *ROCKET NOZZLES
• COLD FLOW
• CONFIGURATIONS
• EXHAUST GASES
• EXPERIMENTAL DATA
• FEASIBILITY STUDIES
• FLEXIBLE STRUCTURES
• GRAPHICS
• NOZZLE GAS FLOW
• PRESSURE
• SOLID PROPELLANT ROCKET ENGINES
• SUPERSONIC FLOW
• SUPERSONIC NOZZLES
• THRUST VECTOR CONTROL SYSTEMS

Subject Categories:

• Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE