Accession Number : AD0839276

Title :   FLEXIBLE EXIT CONE NOZZLE DEVELOPMENT PROGRAM. VOLUME II. COLD FLOW TEST DATA (TABULATED). APPENDIX II.

Descriptive Note : Final rept. 15 Mar 67-31 Jul 68 on Phase 2.

Corporate Author : MORTON THIOKOL INC BRIGHAM CITY UT WASATCH OPERATIONS

Report Date : AUG 1968

Pagination or Media Count : 217

Descriptors :   (*ROCKET NOZZLES, FLEXIBLE STRUCTURES), FEASIBILITY STUDIES, COLD FLOW, COMPUTER PROGRAMS, SUBROUTINES, EXPERIMENTAL DATA, SUPERSONIC FLOW, SUPERSONIC NOZZLES, NOZZLE GAS FLOW, EXHAUST GASES, SOLID PROPELLANT ROCKET ENGINES, PRESSURE, MOVABLE NOZZLES, THRUST VECTOR CONTROL SYSTEMS, TABLES(DATA).

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE