SNAP 19 Viking Program. Bimonthly technical progress report, April-May 1980
Monitoring and evaluation of Viking Lander 1 power system data continued. The RTG series power range as measured at the PCDA was 65 to 67 watts at finroot temperatures between 280/sup 0/F and 310/sup 0/F. The Mars Lander performance history of Viking 1 include both the minimum and maximum data for each of the SOL days. Final available power system data for Viking Lander 2 are shown. Typical SOL day cycles for mission day 1193 are presented. The RTG series power ranged from 69 to 70 watts at finroot temperatures between 270/sup 0/F and 300/sup 0/F. The Mars Lander performance history for Viking 2 is shown. Power system performance data for Pioneer 10 and Pioneer Saturn (initially designated Pioneer 11) were monitored through the reporting period. After adjusting for the telemetry characteristics, the estimated RTG system net power was 114 watts for both Pioneer 10 and Pioneer Saturn.
- Research Organization:
- Teledyne Energy Systems, Timonium, MD (USA)
- DOE Contract Number:
- AC01-80ET32066
- OSTI ID:
- 5193828
- Report Number(s):
- TES-32066-4; ON: DE84010249
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
07 ISOTOPE AND RADIATION SOURCES
070300* -- Isotopic Power Supplies
DATA
DIRECT ENERGY CONVERTERS
ENERGY SYSTEMS
EXPERIMENTAL DATA
INFORMATION
MARS PLANET
MARS SPACE PROBES
NESDPS Office of Nuclear Energy Space and Defense Power Systems
NUMERICAL DATA
PERFORMANCE
PIONEER SPACE PROBES
PLANETS
POWER SYSTEMS
RADIOISOTOPE BATTERIES
SNAP 19 BATTERY
SNAP BATTERIES
SPACE VEHICLES
VEHICLES
VIKING SPACE PROBES
070300* -- Isotopic Power Supplies
DATA
DIRECT ENERGY CONVERTERS
ENERGY SYSTEMS
EXPERIMENTAL DATA
INFORMATION
MARS PLANET
MARS SPACE PROBES
NESDPS Office of Nuclear Energy Space and Defense Power Systems
NUMERICAL DATA
PERFORMANCE
PIONEER SPACE PROBES
PLANETS
POWER SYSTEMS
RADIOISOTOPE BATTERIES
SNAP 19 BATTERY
SNAP BATTERIES
SPACE VEHICLES
VEHICLES
VIKING SPACE PROBES