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KH-8 Gambit 3 : ウィキペディア英語版
KH-8 Gambit 3

The KH-8 (BYEMAN codename Gambit-3)〔(【引用サイトリンク】title=GAMBIT 3 (KH-8) Fact Sheet )〕 was a long-lived series of reconnaissance satellites of the "Key Hole" (KH) series used by the United States from July 1966 to April 1984, and also known as Low Altitude Surveillance Platform.〔( Global Security Space Systems IMINT Overview ) LASP〕 The satellite ejected canisters of photographic film that were retrieved as they descended through the atmosphere by parachute. Ground resolution of the mature satellite system was better than .〔 There were 54 launch attempts of the 3,000 kilogram satellites, all from Vandenberg Air Force Base, on variants of the Titan III rocket. The KH-8 was manufactured by Lockheed. The camera system/satellite was manufactured by Eastman Kodak's A&O Division in Rochester, New York.
The Gambit codename was also used by the satellite's predecessor, the KH-7 Gambit.
Gambit 3 satellites were the same width as the Gambit 1 models, but also slightly longer — reaching about 29 feet (9 m) in length. They carried 12,241 feet (3,731 meters) of film and were designed for longer missions of up to 31 days 〔(【引用サイトリンク】title=Declassified US Spy Satellites from Cold War Land in Ohio )
==Camera Optics Module==

The Camera Optics Module of KH-8 consists of four cameras.
The main camera of KH-8B (introduced in 1971) with a focal length of is a single strip camera, designed to gather high-resolution images of ground targets. In the strip camera the ground image is reflected by a steerable flat mirror to a diameter stationary concave primary mirror. The primary mirror reflects the light through an opening in the flat mirror and through a Ross corrector. At periapsis altitude of 75 nautical miles, the main camera imaged a 6.3 km wide ground swath on a wide moving portion of film through a small slit aperture, resulting in an image scale of 28 meter / millimeter.〔(【引用サイトリンク】title=KH-8 Camera System )〕 The Astro-Position Terrain Camera (APTC) contains three cameras: a 75mm focal length terrain frame camera, and two 90mm 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 degree opposite directions and took images of star fields.〔
The films used by GAMBIT were provided by Eastman Kodak, and evolved through a series of successively higher definition films, starting with Type 3404 with a resolving power of 50 to 100 line pairs per mm.〔(【引用サイトリンク】title=KODAK PLUS-X AERECON II Film 3404 )〕 Subsequent films used were Type 1414 high-definition film, SO-217 high-definition fine-grain film, and a series of films with silver-halide crystals of very uniform size and shape. The size of silver-halide crystals decreased from 1,550 angstrom in film Type SO-315, to 1,200 angstrom in SO-312, and ultimately to 900 angstrom in SO-409.〔(【引用サイトリンク】title=The GAMBIT Story )〕 Under optimal conditions GAMBIT would thus have been able to record ground features as small as 0.28 m to 0.56 m (1 ft to 2 ft) using the Eastman Kodak Type 3404 film. Using a film with a resolving power equivalent to the Kodak's Type 3409 film of 320 to 630 line pairs per mm, GAMBIT would have been able to record ground features as small as 5 cm to 10 cm (2" to 4") .〔(【引用サイトリンク】title=KODAK AERECON High Altitude Film 3409 )〕 The initial September 2011 release of "The Gambit Story" quotes "The mature system produced examples of imagery better than four inches ground-resolution distance". This number was again redacted in a later release.〔 Five to ten centimeters corresponds to the resolution limit imposed by atmospheric turbulence as derived by Fried and, independently, Evvard in the mid-1960s; remarkably, GAMBIT had reached a physical limit on resolution only a few years after the US launched its first reconnaissance satellite. GAMBIT was also able to record objects in orbit. The capability was developed to photograph Soviet spacecraft, but was first used to aid NASA engineers designing repairs for the damaged Skylab space station in 1973.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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