Development of the Small SPT Demo Model

Abstract

This report results from a contract tasking EDB Fakel. as follows: Technical proposal/description of work to achieve the objective of work according to the project it is necessary to solve the following tasks: -To develop, manufacture and test the laboratory model of small SPT with thrust efficiency >0.2 under specific impulses (800-1000s) and power consumption ^100 W. Emphasis will be placed upon maximizing thrust at 100W instead of specific impulse.

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Document Details

Document Type
Technical Report
Publication Date
Mar 16, 2001
Accession Number
ADA393017

Entities

People

  • Boris Arkhipov

Tags

Communities of Interest

  • Autonomy
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Buildings And Structures
  • Contracts
  • Demonstrations
  • Efficiency
  • Energy Consumption
  • Experimental Design
  • Flow
  • Flow Rate
  • Hypervelocity Flow
  • Management Personnel
  • Money
  • Propulsion Systems
  • Safety Equipment
  • Specific Impulse
  • Thrust
  • Thrusters

Readers

  • Aerospace Propulsion Engineering.
  • Software Engineering