Nimbus
2015-05-12 12:53:02.0 [saritz] update PrefLabel (Nimbus-1);
Nimbus-1
Nimbus-1 was launched in August 1964 and was the first in a series of second-generation meteorological research-and-development satellites that was designed to serve as a stabilized, earth-oriented platform for the testing of advanced meteorological sensor systems and for collecting meteorological data. The polar-orbiting spacecraft consisted of three major elements: (1) a sensory ring, (2) solar paddles, and (3) the control system housing. The solar paddles and the control system housing were connected to the sensory ring by a truss structure, giving the satellite the appearance of an ocean buoy. Nimbus-1 was nearly 3.7 m tall, 1.5 m in diameter at the base, and about 3 m across with solar paddles extended. The sensory ring, which formed the satellite base, housed the electronics equipment and battery modules. The lower surface of the torus-shaped sensory ring provided mounting space for sensors and telemetry antennas. An H-frame structure mounted within the center of the torus provided support for the larger experiments and tape recorders. Mounted on the control system housing, which was located on top of the spacecraft, were sun sensors, horizon scanners, gas nozzles for attitude control, and a command antenna. Use of a stabilization and control system allowed the spacecraft's orientation to be controlled to within plus or minus 1 degree for all three axes (pitch, roll, and yaw). The spacecraft carried an advanced vidicon camera system for recording and storing remote cloudcover pictures, an automatic picture transmission camera for providing real-time cloudcover pictures, and a high-resolution infrared radiometer to complement the daytime TV coverage and to measure nighttime radiative temperatures of cloud tops and surface terrain. A short second-stage burn resulted in an unplanned eccentric orbit. Otherwise, the spacecraft and its experiments operated successfully until September 22, 1964. The solar paddles became locked in position, resulting in inadequate electrical power to continue operations. __________ 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: NIMBUS-1 Group: Platform_Identification Platform_Category: Earth Observation Satellites Platform_Series_or_Entity: NIMBUS Short_Name: NIMBUS-1 End_Group Group: Synonymous_Platform_Names Short_Name: NIMBUS-A Short_Name: 00872 End_Group Group: Platform_Associated_Instruments Short_Name: APT NIMBUS-1 Short_Name: HRIR NIMBUS-1 Short_Name: AVCS NIMBUS-1 End_Group Group: Orbit Orbit_Inclination: 98 degrees Period: 98.41999816894531 minutes Perigee: 429.0 km Apogee: 937.0 km Orbit_Type: GEO > Geosynchronous > Geostationary End_Group Creation_Date: 2007-10-11 Online_Resource: http://nssdc.gsfc.nasa.gov/nmc/masterCatalog.do?sc=1964-052A Online_Resource: http://nasascience.nasa.gov/missions/nimbus Online_Resource: http://atmospheres.gsfc.nasa.gov/nimbus/ Group: Platform_Logistics Launch_Date: 1964-08-28 Launch_Site: Vandenberg Air Force Base, USA Primary_Sponsor: USA/NASA End_Group End_Group