Accession Number : AD0831415

Title :   ACCURACY OF RE-ENTRY FLIGHT TEST DATA NEEDED TO DETERMINE RE-ENTRY AERO-THERMODYNAMIC PARAMETERS,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Dore, F. J.

Report Date : 27 JAN 1954

Pagination or Media Count : 19

Abstract : This memorandum establishes accuracy requirements for the various items measured during re-entry for the determination of nose cone aero-thermodynamic parameters. The results are applicable, unless otherwise specified, for a variety of nose cone configurations and re-entry trajectories typical of 7-1, 7-3 and 7-0 missiles. (Author)

Descriptors :   *ATMOSPHERE ENTRY), *THERMAL STRESSES), (*SURFACE TO SURFACE MISSILES, (*NOSE CONES, REENTRY VEHICLES, TELEMETERING DATA, ACCURACY, AERODYNAMIC HEATING, HEAT TRANSFER, LAMINAR BOUNDARY LAYER, ANGLE OF ATTACK, DRAG, SURFACE TEMPERATURE, MATHEMATICAL ANALYSIS, CONICAL BODIES, PRESSURE.

Subject Categories : Surface-launched Guided Missiles
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE