Accession Number:

AD0831415

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Dore, F. J.

Report Date:

1954-01-27

Pagination or Media Count:

19.0

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