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- 20dc9390-40d9-441e-86d2-4ab1e97a276b definition "The Heat Capacity Mapping Mission (HCMM) spacecraft was the first of a series of Applications Explorer Missions (AEM). The objective of the HCMM was to provide comprehensive, accurate, high-spatial-resolution thermal surveys of the surface of the earth. The HCMM spacecraft was made of two distinct modules: (1) an instrument module, containing the heat capacity mapping radiometer and its supporting gear, and (2) a base module, containing the data handling, power, communications, command, and attitude control subsystems required to support the instrument module. The spacecraft was spin stabilized at a rate of 14 rpm. The HCMM circular sun-synchronous orbit allowed the spacecraft to sense surface temperatures near the maximum and minimum of the diurnal cycle. The orbit had a daylight ascending node with nominal equatorial crossing time of 2:00 p.m. Since there was no inclination adjustment capacity, the spacecraft drifted from this crossing time by about 1 hour earlier per year. There was no on-board data storage capability, so only real-time data were transmitted when the satellite came within reception range of seven ground stations. The repeat cycle of the spacecraft was 16 days. Day/night coverage over a given area between the latitudes of 85 deg N and 85 deg S occurred at intervals ranging from 12 to 36 h (once every 16 days). During February 21-23, 1980, the HCMM orbital altitude was lowered from 620 km to 540 km to stop the drift of the orbit plane to unfavorable sun angles which in turn reduced the power collection capability of the solar panels. The operations of the spacecraft were terminated on September 30, 1980. More detailed information can be found in the 'Heat Capacity Mapping Mission Users' Guide' (TRF B30282), available from NSSDC. __________ Taken from the NSSDC System for Information Retrieval and Storage (SIRS). For more information contact the NSSDC Coordinated Request and User Support Office, 301-286-6695 (NASA Goddard Space Flight Center, Code 933.4, Greenbelt, Maryland 20771, USA) Group: Platform_Details Entry_ID: HCMM Group: Platform_Identification Platform_Category: Earth Observation Satellites Short_Name: HCMM Long_Name: Heat Capacity Mapping Mission End_Group Group: Synonymous_Platform_Names Short_Name: HCMM Short_Name: AEM-A Short_Name: Explorer 58 Short_Name: 10818 End_Group Group: Orbit Orbit_Inclination: 97.6 degrees Period: 96.67 min Perigee: 560 km Apogee: 641 km Orbit_Type: LEO > Low Earth Orbit > Polar Sun-Synchronous End_Group Creation_Date: 2007-11-19 Online_Resource: http://nssdc.gsfc.nasa.gov/nmc/masterCatalog.do?sc=1978-041A Sample_Image: http://www.daviddarling.info/images/HCMM.jpg Group: Platform_Logistics Launch_Date: 1978-04-26 Launch_Site: Vandenberg Air Force Base, USA Primary_Sponsor: NASA End_Group End_Group" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b id "1653113" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_id 3466eed1-2fbb-49bf-ab0b-dc08731d502b @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_id b39a69b4-c3b9-4a94-b296-bbbbe5e4c847 @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_id f3261de5-34c1-4980-af22-f9d7e7206d12 @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_label "Earth Observation Satellites" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_label "Platforms" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b path_label "Space-based Platforms" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b prefLabel "HCMM" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b reference "" @default.
- 20dc9390-40d9-441e-86d2-4ab1e97a276b tag "Platforms" @default.
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