The Geodetic and Earth Orbiting Satellite 3 (GEOS-3) was the third in a series of
geodetic missions initiated by NASA. GEOS-3 objectives included defining the structure of
the earth's irregular gravitational field and refining the locations and magnitudes of the
large gravity anomalies, comparing results of the various systems onboard the spacecraft
to determine the most accurate and reliable system, and mapping the ocean surfaces.
The GEOS 3 (Geodynamics Experimental Ocean Satellite) spacecraft was an octahedron,
topped by a truncated pyramid, with a parabolic reflector for a radar altimeter on the
flat bottom side. A metal ribbon boom with end mass extended upward approximately 6.1 m
from the top of the pyramid. Passive laser retroreflector cubes were mounted in a ring
around the parabolic reflector with the normal vector from each cube facing 45 deg outward
from the direction of the earth. A turnstile antenna for VHF and UHF frequencies and
separate antennae for earth-viewing 324 MHz Doppler, C-band, and S-band transponders were
mounted separately on flat surfaces next to the parabolic reflector. The dimension across
the flats of the octahedron was 1.22 m, and the spacecraft was 1.11 m high. Mission
objectives were to perform a satellite altimetry experiment in orbit, to support further
the calibration and position determination of NASA and other agency C-band radar systems,
and to perform a satellite-to-satellite tracking experiment with the ATS 6 spacecraft
using an S-band transponder system. This system was also used for periodic GEOS 3
telemetry data relay through ATS 6, to support further the intercomparison of tracking
systems, to investigate the solid-earth dynamic phenomena through precision laser
tracking, to refine further orbit determination techniques and determine interdatum ties
and gravity models, and to support the calibration and position determination of NASA
Spaceflight Tracking and Data Network (STDN) S-band tracking stations. The following
instrumentation was onboard this spacecraft:
- Two C-Band Antenna
- S-Band Antenna
- ATS/Relay Antenna
- VHF Antenna
- Radar Altimeter
- Doppler Beacon
- Retroreflector array
The retro-reflector array is an annulus with a diameter of 22.5 inches. The annulus
consists of three rows of 264 retro-reflectors inclined at 45 degrees. One of the
retro-reflectors was designed for the infra-red.