Static Force and Moment Tests of the Holloman Narrow-Gage Rocket Sled at Mach Numbers from 1.5 to 4.0

Abstract

Experimental static stability and axial force data are presented for several one-twelfth scale model configurations of a Narrow-Gage Dual-Rail Rocket Sled at Mach numbers from 1.5 to 4.0. The test Reynolds numbers, based on sled base diameter, varied from 0.5 to 1.4 million depending on configuration and/or Mach number. The tests were conducted with the models in close proximity to a ground plane and rail assembly simulating the High Speed Test Track at Holloman Air Force Base. Results are presented showing the effects of configuration variables, such as, nose shape, water brake, water brake trough, bleed area, and sled slipper height and location.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1975
Accession Number
ADA014259

Entities

People

  • J. D. Corce
  • R. H. Rhudy

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Assembly
  • Base Pressure
  • Brakes
  • Clearances
  • Data Reduction
  • Engineering
  • Free Stream
  • Instrumentation
  • Mach Number
  • Measurement
  • New Mexico
  • Rocket Sleds
  • United States
  • Water Brakes
  • Wind Tunnels

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