Launch Success
Liftoff Time (GMT)
12:02:00 AM
Saturday December 22, 1984
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During production of DSP Phase II spacecraft (5-9), Satellites 5 and 6 were stored initially, then retrofitted as 5R and 6R. They featured improved RADEC and primary IR sensors, including the Sensor Evolutionary Development (SED) with 6000 detectors for better resolution and an Above the Horizon (ATH) capability. The addition of Mercury Cadmium Telluride (HgCdTe) detectors enabled a second waveband capability (MWIR). These upgrades increased weight to 1674 kg, with solar panels generating 680 Watts. Despite enhancements, the design life remained at three years. The Phase II Upgrade satellites are distinguished by differences in sensor size and shape, along with unique triangular solar panel paddles.
Geostationary Earth Orbit
1 Payload
1,674 kilograms
Agency
Martin MariettaRocket
Height: 50m
Payload to Orbit
LEO: 14,515 kg
GTO: 5,000 kg
Liftoff Thrust
11,279 Kilonewtons
Fairing
Diameter: 3.05m
Stages
3
Strap-ons
2
142nd
Mission
7th
Mission of 1984
129th
Orbital launch attempt