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KH-8 Gambit-3 (Dual mode, Higherboy)

KH-8 Block 4 [NRO]
KH-8 Gambit-3 (Dual mode) similar

KH-8 Dual mode was a modification of the KH-8 Gambit-3 reconnaissance satellite, which was produced in the early 70ies as a fall-back measure against delay of the area surveillance KH-9 Hexagon satellite. It was also called Higherboy or Highboy.

KH-8 Dual Mode had the same basic layout as the KH-8 (Block 4) 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 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 Block 4 version was a dual platen version, which exposed, independently, both 9-inch and 5-inch film. It provided added versatility to the photographic subsystem by permitting (principally for the 5-inch film) use of other than high-resolution black-and-white film, including experimental films, color film, and false-color infrared. It also provided for adding over 3,800 feet of film for the 5-inch camera.

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.

The spacecraft was built, but placed into storage when the KH-9 succeeded. Eventually it was launched on 21. January 1982 on a Titan-3(24)B Agena-D booster into an orbit with a much higher apogee than the KH-8 satellites. It performed area imaging from the initial orbit and later lowered the orbit for high resolution imaging.

One of the two reentry vehicles failed to return to earth properly. This launch represented a mystery over several years and was mostly attributed to a test flight of the project Indigo radar satellite, which in fact never happened. Four objects from this satellite, originally thought to be subsatellites, were associated with the failed return vehicle, as the internal container separated from the heatshield and thrust cone.

The second reentry vehicle returned to earth, but the film was degraded.

Nation: USA
Type / Application: Reconnaissance, photo
Operator: USAF
Contractors:
Equipment: ?
Configuration: Agena-D
Propulsion: Bell 8096, SPS
Power: 2 deployable solar arrays, batteries
Lifetime: 122 days
Mass:
Orbit: 630 km × 641 km, 97.3 (initial); 137 km × 527 km, 97.3 (later)
Satellite COSPAR Date LS Launch Vehicle Remarks
KH-8 52 (Gambit-3 4352, OPS 2849) 1982-006A 21.01.1982 Va SLC-4W Titan-3(24)B Agena-D