S3 1 [USAF]
S3 (Small Secondary Satellites) were launched as piggy back payloads on some KH-9 spysat launches. Each one had his own solid fuel motor to perform injection into an higher orbit.
S3 1 carried eigth complementary types of experiments, designed to study atmospheric density and its changes at low altitudes:
The satellite was spin stabilized, with the spin axis perpendicular to its polar orbit. Orbit precession, when the orbit is inclined more than 70 deg, was limited to less than 0.5 deg per day. This limited observations for sampling to less than one-fourth of the possible 25 h of local time over the 7-month satellite lifetime.
S3 2 carried following set of instruments:
S3 3 was a small observatory in a near-polar orbit with eight different sensors on board. It was designed to observe various magnetospheric parameters and their interrelationships. Sensors, which observed energetic protons and Alpha particles, also provided real-time observations for use by the U.S. Air Force Air Weather Service. It carried following set of instruments:
|Type / Application:||Experimental|
|Operator:||US Air Force (USAF) STP (Space Test Program)|
|Propulsion:||Star-17 (#1), Star-13A (#2), Star-17A (#3)|
|Power:||Solar cells, batteries|
|Mass:||276 kg kg (#1)|
|Orbit:||148 km × 3483 km, 96.99° (#1); 233 km × 1544 km, 96.28° (#2); 232 km × 6038 km, 97.46° (#3)|
|S3 1 (S73-5, OPS 8452)||1974-085C||29.10.1974||Va SLC-4E||Titan-3D||with KH-9 9, Raquel 1|
|S3 2 (S73-6, OPS 5547)||1975-114B||04.12.1975||Va SLC-4E||Titan-3D||with KH-9 11|
|S3 3 (S74-2, OPS 3986)||1976-065B||08.07.1976||Va SLC-4E||Titan-3D||with KH-9 12, Ursala 3|