Feasibility of Optimizing Nozzle Performance for Orbital-Launch Nuclear Rockets

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1963
Accession Number
ADA396913

Entities

People

  • John R. Jack

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Cooling
  • Equations
  • Flow Rate
  • Gas Turbine Nozzles
  • Geometry
  • Heat Flux
  • Heat Loss
  • Heat Transfer
  • Heat Transfer Coefficients
  • Nozzles
  • Power Levels
  • Radiation
  • Rocket Nozzles
  • Specific Impulse
  • Stagnation Pressure
  • Temperature Gradients
  • Thermal Radiation

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites