MATHEMATICAL MODEL AND COMPUTER PROGRAM FOR THE ASCENT AND DESCENT OF HIGH-ALTITUDE TETHERED BALLOONS. SCHEDULE SUB-LINE ITEM 1AD

Abstract

The results of the preliminary study indicate that it is feasible to launch and retrieve high-altitude balloons under certain conditions. It was shown that a 30 million cu ft balloon can be launched in a Summer I-75 percent wind profile at 2000 ft/min, and retrieved in the same wind at -200 ft/min with 20 percent of the helium valved off. Although launch and retrieval are possible in the Winter I wind profile, it is more restricted. The 79 million cu ft balloon in the Winter I 25 percent wind show results similar to the 30 million cu ft balloon in the Summer I 75 percent wind. The results of the feasibility study can be used as preliminary design criteria for components of the tethered balloon-systems-balloon, tether and winch.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1968
Accession Number
AD0672735

Entities

People

  • George R. Doyle Jr.
  • Jerome J. Vorachek

Organizations

  • Goodyear Aerospace

Tags

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Atmospheric Density
  • Center Of Gravity
  • Computer Programs
  • Computer Simulations
  • Computers
  • Descent Trajectories
  • Dynamic Pressure
  • Equations Of Motion
  • Feasibility Studies
  • High Altitude
  • Mathematical Models
  • Operating Systems
  • Sea Level
  • Simulations
  • Wind Velocity

Fields of Study

  • Environmental science

Readers

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