Feasibility of demonstration solar dynamics on space station

Intersociety Energy Conversion Engineering Conference, 1994

Volumn , Issue , 1994, Pages 613-618

  Hanlon, Casey ^a  

^a NYMA Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BRAYTON CYCLE; CONCENTRATION (PROCESS); COST ACCOUNTING; DIFFUSERS (OPTICAL); ENERGY CONVERSION; ENGINES; INTEGRATION; NASA; SOFTWARE TESTING; SOLAR CELL ARRAYS; SPACE STATIONS; THERMOANALYSIS; COMPUTATIONAL METHODS; SOLAR ENERGY; SPACE FLIGHT;

BRAYTON ROTATING UNITS; CLOSED BRAYTON CYCLE; CYCLE PERFORMANCE; ELECTRICAL POWER; INTEGRATION ISSUES; SOLAR DYNAMIC; STRUCTURAL INTEGRATION; THERMO DYNAMIC ANALYSIS;

COST BENEFIT ANALYSIS; SPACECRAFT POWER SUPPLIES;

BRAYTON ISOTOPE POWER SYSTEM PROGRAM; SOLAR DYNAMIC DEMONSTRATOR;

EID: 0028758107     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1994-4199     Document Type: Conference Paper

References (6)

1. l. Kesseli, B, Saunders, R. I. and Gatchelder, G., "The Advanced Heat Receiver Conceptual Design Study". NASA-CR-182 177, Sanders Associates, Oct., 1988.
2. Solar Dynamic Design Description, Rockwell International document No. EID-00787, April 02, 1991.
3. Task Order 7, Space Station Freedom Growth Options Final Report, Pg 6, Jan 13, 1992. Rocketdyne Engineering.
4. Power System Description Document, DR: SE-02, 15 Dec. 1992. Rockwell International, Rocketdyne Division, Canoga Park, Ca.
5. Space Station Active Thermal Control System Evolution, 1992 Annual Report, Pg 3. Lockheed Engineering & Sciences Company, Dec. 1992.
6. Task Order 7, Space Station Freedom Growth Options Final Report, Pg 6, Jan 13, 1992. Rocketdyne Engineering.