KH-8 48 [USAF]
KH-8 or Gambit-3 was the second generation of Gambit high resolution reconnaissance satellites. The KH-8 Block 3 were the third iteration of this design, introducing an improved roll joint.
KH-8 Block 3 had the same basic layout as the KH-8 (Block 2) series. The forward part was joint via a roll joint with the Agena-D. The major subsystems of the satellite included a photographic-payload section (PPS), a satellite-control section (SCS), and the booster vehicle. The payload section contained a camera module and two satellite recovery-vehicles (SRV). The control section included the command system, the orbit-adjust module, an attitude-control subsystem, a back-up stabilization system (BUSS), and the power supply.
The next 11 satellites of the KH-8 Block 3 series (KH-8 37 to 47) featured an improved roll joint capable of 18000 maneuvers per mission,increasing greatly the agility of the imaging system. Also the film capacity was increased. The block 3 satellites were able to perform satellite-to-satellite (SSquared) imaging.
The camera system was strip camera coupled to an optical system a focal length of 4.46 m. In the optical system the ground image is reflected by a steerable flat mirror to a 1.21 m diameter stationary concave primary mirror. The primary mirror reflects the light through an opening in the flat mirror and through a Ross corrector. At perigeum, the main camera imaged a 6.3 km wide ground swath on a 223.8 mm wide moving portion of film through a small slit aperture. The ground resolution was as small as 0.1 m or better, near the theoretical physical e resolution limit imposed by atmospheric turbulence.
The Astro-Position Terrain Camera (APTC) contained three cameras: a 75 mm focal length terrain frame camera, and two 90 mm focal length stellar cameras. The terrain frame camera takes exposures of Earth in direction of the vehicle roll position for attitude determination. The stellar cameras observed in 180° opposite directions and took images of star fields.
This series used the stretched Titan-3(24)B Agena-D version as launch vehicle.
KH-8 39 was lost due to fuel valve failure of the Agena during ascent.
The KH-8 Block-3 satellites were succeeded by the improved KH-8 Block 3 satellites featuring a number of improvements, including solar arrays.
|Type / Application:||Reconnaissance, photo (film return type)|
|Configuration:||Agena-D, 2 SRVs|
|Propulsion:||Bell 8096, SPS|
|Lifetime:||30 to 45 days|
|KH-8 37 (Gambit-3 4337, OPS 3978)||1972-103A||21.12.1972||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 38 (Gambit-3 4338, OPS 2093)||1973-028A||16.05.1973||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 39 (Gambit-3 4339, OPS 4018)||1973-F04||26.06.1973||Va SLC-4W||F||Titan-3(24)B Agena-D|
|KH-8 40 (Gambit-3 4340, OPS 6275)||1973-068A||27.09.1973||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 41 (Gambit-3 4341, OPS 6889)||1974-007A||13.02.1974||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 42 (Gambit-3 4342, OPS 1776)||1974-042A||06.06.1974||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 43 (Gambit-3 4343, OPS 3004)||1974-065A||14.08.1974||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 44 (Gambit-3 4344, OPS 4883)||1975-032A||18.04.1975||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 45 (Gambit-3 4345, OPS 5499)||1975-098A||09.10.1975||Va SLC-4W||Titan-3(24)B Agena-D|
|KH-8 46 (Gambit-3 4346, OPS 7600)||1976-027A||22.03.1976||Va SLC-4W||Titan-3(24)B Agena-D .|
|KH-8 47 (Gambit-3 4347, OPS 8533)||1976-094A||15.09.1976||Va SLC-4W||Titan-3(24)B Agena-D|