SOLAR THERMOELECTRIC GENERATOR SYSTEM CONCEPT AND FEASIBILITY STUDY.

Abstract

The feasiblity of combining concentrated solar energy, thermal storage, and a thermoelectric generator as a power supply for space applications has been proven. A nominal 14 watt model, for operation in a 300 mile earth orbit, has been fabricated, tested using electric heat input in an altitude chamber, tested using natural solar energy input in an earth atmosphere and operated on a life test. A 90 minute orbit with 55 minutes of energy input, or sunlight, and 35 minutes of darkness has been simulated. The generator produced constant power (= 7%) for the full 90 minutes. Practical factors obtained from the feasibility model testing have been incorporated into an analytical investigation of a complete system. A power-to-weight ratio of 2.4 is attainable at a power level of 70 watts using a present day 5 foot diameter collector concentrator. The system efficiency (power output from the generator vs. solar energy intercepted) of 4.3% is produced with a thermopile producing 13 watts per pound. Thirty eight (38) per cent of the system weight is provided by the collector concentrator. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1964
Accession Number
AD0430127

Entities

Organizations

  • Westinghouse Electric Corporation

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accumulators
  • Altitude Chambers
  • Earth Orbits
  • Energy
  • Feasibility Studies
  • Generators
  • Life Tests
  • Orbits
  • Power Levels
  • Power Supplies
  • Solar Energy

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Solar Photovoltaics and Thermoelectric Devices.
  • Space Exploration and Orbital Mechanics.

Technology Areas

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