GEOS-3

From Wikipedia, the free encyclopedia
Jump to: navigation, search
GEOS-3
Geos-3.gif
GEOS-3
Mission type Geodesy
Operator NASA
COSPAR ID 1975-027A
SATCAT № 7734
Website ilrs.gsfc.nasa.gov
Spacecraft properties
Spacecraft type GEOS
Manufacturer JHU / APL
Launch mass 346 kilograms (763 lb)
Dimensions 1.32 by 0.81 meters (4.3 ft × 2.7 ft)
6 meters (20 ft) long with boom deployed
Start of mission
Launch date 9 April 1975, 23:58:02 (1975-04-09UTC23:58:02Z) UTC[1]
Rocket Delta 1410
Launch site Vandenberg SLC-2W
Contractor NASA
End of mission
Deactivated July 1979
Orbital parameters
Reference system Geocentric
Regime Low Earth
Semi-major axis 7,208.68 kilometers (4,479.27 mi)
Eccentricity 0.001273
Perigee 828 kilometers (514 mi)
Apogee 846 kilometers (526 mi)
Inclination 114.98 degrees
Period 101.52 minutes
Epoch 14 January 2014, 03:51:02 UTC[2]
Instruments
  • Radar altimeter (ALT)
  • Retroreflector array (RRA)
  • Doppler beacon
  • S-band antenna
  • C-band antenna (Two)
  • SST Tracking

GEOS-3, or Geodynamics Experimental Ocean Satellite 3, or GEOS-C, was the third and final satellite as part of NASA's Geodetic Earth Orbiting Satellite/Geodynamics Experimental Ocean Satellite program (NGSP) to better understand and test satellite tracking systems.[3] For, GEOS mission 1 and 2, GEOS referred to Geodetic Earth Orbiting Satellite but was changed to Geodynamics Experimental Ocean Satellite for the GEOS-3 satellite[3]

Introduction[edit]

The satellite mission was designed to further an understanding of the earth’s gravitational field, size and shape of the terrestrial geoid, deep ocean tides, sea state, current structure, crustal structure, solid earth dynamics, and remote sensing technology.[4] Jerome Rosenburg at NASA Headquarters initiated the GEOS-3 project in 1970.[4] The project was to serve as a stepping stone between the GEOS program and the emerging NASA Earth and Ocean Physics Application Program.[4] GEOS-1 and GEOS-2 had provided useful information about the structure of the earth’s gravitational field, but new technology was deemed necessary to gain a further understanding.[4] The project was initially cancelled due to budgetary concerns after an initial 1-year study, but was re-instated in late 1971.[4] The satellite was launched in April 9, 1975 and remained operational until late July 1979.[5]

Instruments[edit]

The following is a list of instruments/systems that were onboard or part of the GEOS-3 satellite, including a description of their general purpose:[4][6]

  • Radar Altimeter (ALT) - A multimode radar system with the ability to provide precise satellite-to-ocean surface height measurements. The radar system provided global and intensive data gathering modes, which could provide height precision measurements at 50 cm and 20 cm respectively.
  • Retroreflector Array (RRA) - A system consisting of a ground-based laser and a space borne retroreflector. This laser emitter-detector system provided satellite-ranging data.
  • Doppler System - A system of dual frequency space borne doppler beacons at 162 and 324 MHz and a ground-based receiver station. This system was used to measure the effects of first-order ionospheric refraction and make corrections to the Doppler frequency.
  • S-band Tracking System - A tracking system which had three modes of operations for satellite to satellite tracking, ground-station tracking, and direct unified S-band.
  • C-band System - A system of two C-band radar transponders used to better understand the accuracies of the gravimetric and geometric measurements. The system also supported the altimeter and C-band calibration.
  • Satellite-to-Satellite Tracking (SST) - The SST experiment consisted of, the ground-based ATS ranging system, the wideband communication transponder on the ATS-6 geosynchronous spacecraft, and the ranging transponder on the LEO satellite.

Impacts on the Scientific Community[edit]

The GOES-3 mission provided data that furthered scientific understanding in various fields. The ocean height data set from this mission provided the first comprehensive coverage in most areas of the world’s ocean’s, providing a better understanding of the Ocean Geoid.[4] Ocean height also provided information about quasi-stationary departures from the geoid, for events like currents, eddies, storm surges, etc.[4] The return waveform data was used to better understand the sea state at a level that was comparable to buoy-collected data.[4] An unexpected result was the ability to use waveform data to derive surface wind speed, and the ability to maintain track over terrain and ice[4] Altimeter data from GEOS-3 has been utilized by many gravity models, including GEM-T3, JGM-1 and JGM-2 [5]


References[edit]

  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 14 January 2014. 
  2. ^ "GEOS 3 Satellite details 1975-027A NORAD 7734". N2YO. 14 January 2014. Retrieved 14 January 2014. 
  3. ^ a b "NASA - GEOS Program". eoPortal Directory. Retrieved 8 December 2013. 
  4. ^ a b c d e f g h i j Stanley, H. R. (30 July 1979). "The GEOS 3 Project". Journal of Geophysical Research 84: 3779–3783. doi:10.1029/JB084iB08p03779. 
  5. ^ a b "GEOS-3". JPL. Retrieved 8 December 2013. 
  6. ^ "GEOS 3". International Laser Ranging Service. Retrieved 8 December 2013.