Design, Development and Flight Test of the Super Loki Stable Booster Rocket Systems

Abstract

The Super Loki stable booster rocket systems have been developed to obtain high altitude temperature, density, and wind measurements by means of small inexpensive rocket systems which have post-burnout stable booster trajectories. These systems can be used at ranges where booster wind drift is a safety problem. The expended rocket booster impacts at a range of about 15,000 feet or 2.46 nautical miles from the launch site. These systems have been developed to replace the Super Loki PWN-10A, PWN-10B, and PWN-12A at launch sites requiring either transponder or falling sphere payloads and stable booster impacts.

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1973
Accession Number
AD0766737

Entities

People

  • Bruce Bollermann
  • Robert L. Walker

Tags

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Ammonium Perchlorate
  • Ballistic Trajectories
  • Booster Rocket Engines
  • Center Of Gravity
  • Classification
  • Coefficients
  • Combustion
  • High Altitude
  • Launch Vehicles
  • Leading Edges
  • Measurement
  • Rocket Engines
  • Rockets
  • Sea Level
  • Transmitters

Readers

  • Aerospace Test and Evaluation
  • Atmospheric Science/Meteorology
  • Control Systems Engineering.