Tophat 1 [NSA]
The Tophat satellites were part of a series of so called Program 11 or P-11 "Subsatellite Ferrets", low orbit ELINT/SIGINT satellites to pinpoint and characterize different Radar emitters in the Soviet Union and Warsaw pact states.
The Tophat communications intelligence (COMINT) payloads were used to intercept communications signals in the 450–1000 MHz range.
The satellites were based on Lockheed's P-11 bus, which was designed to fit on the aft rack of the Agena-D upper stage or later on a rack on the KH-9 Hexagon reconnaissance satellite. The bus contained each one or two focused payload black boxes and different antenna configurations according to payload, as well as deployable solar arrays. The satellite featured two solid rocket motors, which allowed them to rise and circularize their orbit after deployment from the host satellite. Both spin or gravity gradient stabilization was possible.
These subsatellites were deployed from the propulsion rack of the Agena-D stage of a KH-4B Corona or directly from a KH-9 Hexagon reconnaissance satellites. They used two solid-fuel kick-motors to maneuver themselves into their operational orbits after deployment.
|Type / Application:||SIGINT, COMINT|
|Operator:||US Air Force (USAF)|
|Contractors:||Lockheed (bus); Ling Tempco Vought → E-Systems (payload)|
|Power:||Solar cells, batteries|
|Lifetime:||9 months (planned); 44 month reached (#1)|
|Orbit:||478 km × 508 km, 83.19° (#1); 501 km × 528 km, 94.00° (#2)|
|Tophat 1 (P-11 4423, Mission 7334, OPS 6829)||1970-098B||18.11.1970||Va SLC-3W||Thorad-SLV2H Agena-D||with KH-4B 12|
|Tophat 2 (P-11 4428, Mission 7340, OPS 4547)||1974-020C||10.04.1974||Va SLC-4E||Titan-3D||with KH-9 8, IRCB|