SPACE POWER SYSTEMS.  PART I.

SPACE POWER SYSTEMS. PART I.

Active / Technical Report | Accession Number: AD0698652 |

Abstract:

Contents Power requirements, similitudes and limitations in trans-conventional propulsion systems Space power systems Nuclear space power systems Nuclear space power systems, Reactor space power systems, Radioisotope space power Mechanical heat engines for space power systems.

Author(s):

No Author(s) Identified

Author Organization(s):

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Supplementary Note:

NATO furnished. See also Part 2, AD-698 653. Presented by the Propulsion and Energetics Panel and the Consultant and Exchange Programme of the Advisory Group for Aerospace Research and Development, at Universite' Libre de Bruxelles, Belgium, 2-6 Oct 67.

Pagination:

0349

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

AGARD-ograph-123-Pt-1

Subject Terms

Joint Capability Areas:

JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means

Communities of Interest:

Energy and Power Technologies

Descriptor(s):

(*SPACE PROPULSION, SYMPOSIA), HEAT ENGINES, SPACECRAFT NUCLEAR PROPULSION, SOLAR ROCKETS, SOLAR CELLS, FUEL CELLS, ENERGY CONVERSION, RANKINE CYCLE, THERMIONIC CONVERTERS, THERMOELECTRICITY, TURBINES, BRAYTON CYCLE, ELECTROCHEMISTRY, ION ENGINES, SOLAR RADIATION, POWER SUPPLIES, OPTIMIZATION, STATE OF THE ART REVIEWS, BELGIUM

Field(s)/Group(s):

Non-electrical Energy Conversion, Nuclear Propulsion, Unmanned Spacecraft

Keyword(s):

AC GENERATORS, RADIOISOTOPE HEAT SOURCES, SNAP

Report Date:

1969 Nov 01