MULTI-TUBE BOILER AND CONDENSER CAPSULE.

Abstract

The recommended design of an experimental system to evaluate the performance of an orbital organic multi-tube boiler and condenser capsule is presented. The system will have characteristics identical to an isotope-powered system with the exception of: (a) an electrical heat source is used in place of an isotope heat source and (b) a nozzle is used in place of a turboalternator unit. The experiment will provide critical zero gravity information on two-phase thermodynamics and hydrodynamics typical of a Rankine space power system. An important aspect of the system is its dual radiator-condensers. One condenser is designed to operate in a 1 g acceleration environment (flow 'upward') to guarantee orbital stability. The second is designed to operate at 1.0 psia inlet pressure in order to simulate operation of a high efficiency system and to permit the condenser margin of stability to be parametrically evaluated. Both condensers will be operated consecutively in orbit. The system is composed of a flash-type, electrically heated, parallel tube boiler; a choked nozzle for turbine simulation; a compact regenerator; dual direct radiator-condensers; dual condenser pressure regulating tanks; state-of-the-art pumping system; batteries; electrical controls; instrumentation; telemetry; and associated structure.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1967
Accession Number
AD0813049

Tags

DTIC Thesaurus Topics

  • Efficiency
  • Energy
  • Environment
  • Guarantees
  • Heat Energy
  • Hydrodynamics
  • Instrumentation
  • Physics
  • Simulations
  • Telemetry
  • Thermodynamics

Fields of Study

  • Engineering
  • Physics

Readers

  • Control Systems Engineering.
  • Electrical Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster