Aspheric reflector with five-element Ross corrector
Diameter
1.1 m (3 ft 7 in)
Focal length
4.46 m (14.6 ft)
Focal ratio
f/4.09
Wavelengths
visible light, Near-infrared
Instruments
MC
Main Camera
APTC
Astro-Position Terrain Camera
The KH-8 (BYEMAN codename Gambit-3)[1] 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,[2] and also known as Low Altitude Surveillance Platform.[3] The satellite ejected "film-bucket" 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 4 inches (0.10 m).[4] There were 54 launch attempts of the 3,000 kilogram satellites, all from Vandenberg Air Force Base, on variants of the Titan III rocket. Three launches failed to achieve orbit. The first one was satellite #5 on April 26, 1967, which fell into the Pacific Ocean after the Titan second stage developed low thrust. The second was satellite #35 on May 20, 1972, which suffered an Agena pneumatic regulator failure and reentered the atmosphere. A few months later, pieces of the satellite turned up in England and the US managed to arrange for their hasty return. The third failure was satellite #39 on June 26, 1973, which suffered a stuck Agena fuel valve. The Bell 8096 engine failed to start and the satellite burned up in the atmosphere. 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 (8.8 m) in length. They carried 12,241 feet (3,731 meters) of film and were designed for longer missions of up to 31 days.[5]
While Gambit was primarily designed and operated as a surveillance satellite, capturing high definition images of specific targets at low orbital altitudes, a single Gambit Block 3 mission was operated in 'dual-mode', orbiting first at a higher altitude to capture wide-area search imagery before lowering its perigee to capture normal surveillance imagery. The first film return capsule failed to separate correctly due to a new pyro mechanism failing to perform correctly. The contingency release mechanism separated the film bucket and parachute from its return capsule, and left the film bucket stranded in orbit. In September 2002, the film bucket re-entered over the South Atlantic into deep water. As the film bucket lacked its protective heatshield or the parachute needed to slow its descent, no attempt was made to recover it.[6]
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 175.6 in (4.46 m) 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 1.21 m (48 in) 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 (139 km), the main camera imaged a 6.3 km wide ground swath on a 8.811 in (223.8 mm) wide moving portion of film through a small slit aperture, resulting in an image scale of 28 meter / millimeter.[7][8] 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.[7]
Ground-resolution distance achievable by KH-8
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.[9] 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.[4] Under optimal conditions GAMBIT would thus have been able to record ground features as small as 0.28 to 0.56 m (0.92 to 1.84 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").[10] 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.[4] Five to ten centimeters corresponds to the resolution limit imposed by atmospheric turbulence as derived by Fried[11] and, independently, Evvard[12] 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.[13][14]
Missions
[edit]Ascent and Orbital events for GAMBIT-3 missionsN1 (rocket) imaged by KH-8 Gambit on 19 September 1968KH-8 GAMBIT 3 (Block 1) main featuresKH-8 GAMBIT 3 (Block 2) main featuresKH-8 GAMBIT 3 (Block 3 & 4) main features
Name
Block[15]
Launch Date
Alt. Name
NSSDC ID No.
Launch Vehicle
Orbit
Decay date
KH8-1
I
1966-07-29
OPS-3014
1966-069A
Titan IIIB
158.0 km × 250.0 km, i=94.1°
1966-08-06[16]
KH8-2
I
1966-09-28
OPS-4096
1966-086A
Titan IIIB
KH8-3
I
1966-12-14
OPS-8968
1966-113A
Titan IIIB
KH8-4
I
1967-02-24
OPS-4204
1967-016A
Titan IIIB
KH8-5
I
1967-04-26
OPS-4243
1967-F04, 1967-003X
Titan IIIB
no stable orbit
1967-04-26
KH8-6
I
1967-06-20
OPS-4282
1967-064A
Titan IIIB
KH8-7
I
1967-08-16
OPS-4886
1967-079A
Titan IIIB
KH8-8
I
1967-09-19
OPS-4941
1967-090A
Titan IIIB
KH8-9
I
1967-10-25
OPS-4995
1967-103A
Titan IIIB
KH8-10
I
1967-12-05
OPS-5000
1967-121A
Titan IIIB
KH8-11
I
1968-01-18
OPS-5028
1968-005A
Titan IIIB
KH8-12
I
1968-03-13
OPS-5057
1968-018A
Titan IIIB
KH8-13
I
1968-04-17
OPS-5105
1968-031A
Titan IIIB
KH8-14
I
1968-06-05
OPS-5138
1968-047A
Titan IIIB
KH8-15
I
1968-08-06
OPS-5187
1968-064A
Titan IIIB
KH8-16
I
1968-09-10
OPS-5247
1968-074A
Titan IIIB
KH8-17
I
1968-11-06
OPS-5296
1968-099A
Titan IIIB
KH8-18
I
1968-12-04
OPS-6518
1968-108A
Titan IIIB
KH8-19
I
1969-01-22
OPS-7585
1969-007A
Titan IIIB
KH8-20
I
1969-03-04
OPS-4248
1969-019A
Titan IIIB
KH8-21
I
1969-04-15
OPS-5310
1969-039A
Titan IIIB
KH8-22
I
1969-06-03
OPS-1077
1969-050A
Titan IIIB
KH8-23
II
1969-08-23
OPS-7807
1969-074A
Titan 23B
KH8-24
II
1969-10-24
OPS-8455
1969-095A
Titan 23B
KH8-25
II
1970-01-14
OPS-6531
1970-002A
Titan 23B
KH8-26
II
1970-04-15
OPS-2863
1970-031A
Titan 23B
KH8-27
II
1970-06-25
OPS-6820
1970-048A
Titan 23B
KH8-28
II
1970-08-18
OPS-7874
1970-061A
Titan 23B
KH8-29
II
1970-10-23
OPS-7568
1970-090A
Titan 23B
KH8-30
II
1971-01-21
OPS-7776
1971-005A
Titan 23B
139.0 km × 418.0 km, i=110.8°
1971-02-09[17]
KH8-31
II
1971-04-22
OPS-7899
1971-033A
Titan 23B
132.0 km × 401.0 km, i=110.9°
1971-05-13[18]
KH8-32
II
1971-08-12
OPS-8607
1971-070A
Titan 24B
137.0 km × 424.0 km, i=111.0°
1971-09-03[19]
KH8-33
II
1971-10-23
OPS-7616
1971-092A
Titan 24B
134.0 km × 416.0 km, i=110.9°
1971-11-17[20]
KH8-34
II
1972-03-17
OPS-1678
1972-016A
Titan 24B
131.0 km × 409.0 km, i=111.0°
1972-04-11[21]
KH8-35
II
1972-05-20
OPS-6574
1972-F03
Titan 24B
failed to reach orbit
KH8-36
II
1972-09-01
OPS-8888
1972-068A
Titan 24B
140.0 km × 380.0 km, i=110.5°
1972-09-30[22]
KH8-37
III
1972-12-21
OPS-3978
1972-103A
Titan 24B
139.0 km × 378.0 km, i=110.5°
1973-01-23[23]
KH8-38
III
1973-05-16
OPS-2093
1973-028A
Titan 24B
139.0 km × 399.0 km, i=110.5°
1973-06-13[24]
KH8-39
III
1973-06-26
OPS-4018
1973-F04
Titan 24B
failed to reach orbit
(mix-up with KH8-38 in NSSDC)
KH8-40
III
1973-09-27
OPS-6275
1973-068A
Titan 24B
131.0 km × 385.0 km, i=110.5°
1973-10-29[25]
KH8-41
III
1974-02-13
OPS-6889
1974-007A
Titan 24B
134.0 km × 393.0 km, i=110.4°
1974-03-17[26]
KH8-42
III
1974-06-06
OPS-1776
1974-042A
Titan 24B
136.0 km × 394.0 km, i=110.5°
1974-07-24[27]
KH8-43
III
1974-08-14
OPS-3004
1974-065A
Titan 24B
135.0 km × 402.0 km, i=110.5°
1974-09-29[28]
KH8-44
III
1975-04-18
OPS-4883
1975-032A
Titan 24B
134.0 km × 401.0 km, i=110.5°
1975-06-05[29]
KH8-45
III
1975-10-09
OPS-5499
1975-098A
Titan 24B
125.0 km × 356.0 km, i=96.4°
1975-11-30[30]
KH8-46
III
1976-03-22
OPS-7600
1976-027A
Titan 24B
125.0 km × 347.0 km, i=96.4°
1976-05-18[31]
KH8-47
III
1976-09-15
OPS-8533
1976-094A
Titan 24B
135.0 km × 330.0 km, i=96.4°
1976-11-05[32]
KH8-48
IV
1977-03-13
OPS-4915
1977-019A
Titan 24B
124.0 km × 348.0 km, i=96.4°
1977-05-26[33]
KH8-49
IV
1977-09-23
OPS-7471
1977-094A
Titan 24B
125.0 km × 352.0 km, i=96.5°
1977-12-08[34]
KH8-50
IV
1979-05-28
OPS-7164
1979-044A
Titan 24B
124.0 km × 305.0 km, i=96.4°
1979-08-26[35]
KH8-51
IV
1981-02-28
OPS-1166
1981-019A
Titan 24B
138.0 km × 336.0 km, i=96.4°
1981-06-20[36]
KH8-52
IV
1982-01-21
OPS-2849
1982-006A
Titan 24B
630.0 km × 641.0 km, i=97.4°
1982-05-23[37]
KH8-53
IV
1983-04-15
OPS-2925
1983-032A
Titan 24B
124.0 km × 254.0 km, i=96.5°
1983-08-21[38]
KH8-54
IV
1984-04-17
OPS-8424
1984-039A
Titan 24B
127.0 km × 235.0 km, i=96.4°
1984-08-13[39]
(NSSDC ID Numbers: See COSPAR)
Notable Missions
[edit]
In May 1973 Gambit KH8-38 was used to observe the crippled Skylab space station, as part of the preparation for repairing it by the Skylab 2 mission.[14]
Cost
[edit]
The total cost of the 54 flight KH-8 program from FY1964 to FY1985, without non-recurring costs, was US$2.3 billion in respective year dollars.[15]
Other U.S. imaging spy satellites
[edit]
Corona series: KH-1, KH-2, KH-3, KH-4
KH-5 ARGON, KH-6 LANYARD
KH-7 Gambit and KH-8 GAMBIT
KH-9 Hexagon "Big Bird"
MOL – KH-10
KH-11 Kennen, Misty (classified project), Enhanced Imaging System
References
[edit]
Mark Wade (August 9, 2003). KH-8. Encyclopedia Astronautica. Accessed April 23, 2004.
KH-8 Gambit. GlobalSecurity.org
^"GAMBIT 3 KH-8 Reconnaissance Satellite". National Museum of the U.S. Air Force. Retrieved August 10, 2022.
^Richelson, Jeffrey (1987). American espionage and the Soviet target. W. Morrow. p. 195. ISBN 978-0-688-06753-3.
^Global Security Space Systems IMINT Overview LASP
^ abc"The GAMBIT Story". National Reconnaissance Office. June 1991. Archived from the original on September 15, 2012. Retrieved September 26, 2011.
^"Declassified US Spy Satellites from Cold War Land in Ohio". Space.com. January 28, 2012. Retrieved October 11, 2015.
^"GAMBIT_Dual_Mode". www.nro.gov. Archived from the original on April 14, 2023. Retrieved February 19, 2021.
^ ab"KH-8 Camera System". National Reconnaissance Office. 1970. Archived from the original on September 15, 2012. Retrieved September 26, 2011.
^Day, Dwayne A. (November 29, 2010). "Ike's gambit: The development and operations of the KH-7 and KH-8 spy satellites". www.thespacereview.com. Retrieved January 25, 2009.
^"KODAK PLUS-X AERECON II Film 3404" (PDF). Kodak. November 28, 2005. Archived from the original (PDF) on November 6, 2013.
^"KODAK AERECON High Altitude Film 3409" (PDF). Kodak. November 28, 2005. Archived from the original (PDF) on January 10, 2014.
^Fried, David (1966). "Limiting Resolution Looking Down Through the Atmosphere". Journal of the Optical Society of America. 56 (10): 1380–1384. Bibcode:1966JOSA...56.1380F. doi:10.1364/josa.56.001380.
^Evvard, John (December 1, 1968). "Atmospheric Turbulence Limits on the Observational Capabilities of Aerospacecraft". NASA Technical Note. NASA-TN-D-4940. Retrieved June 18, 2015.
^Day, Dwayne Allen (June 11, 2012). "Out of the black". The Space Review. Retrieved June 11, 2012.
^ abDay, Dwayne (May 20, 2013). "Those magnificent spooks and their spying machine: The spies help rescue Skylab". The Space Review. Retrieved July 10, 2020.
^ ab"The GAMBIT story". National Reconnaissance Office. June 1991. Archived from the original on October 7, 2017. Retrieved September 25, 2011.
^"KH 8-01". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-30". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-31". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-32". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-33". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-34". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-36". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-37". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-38". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-40". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-41". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-42". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-43". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-44". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-45". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-46". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-47". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-48". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-49". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-50". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-51". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-52". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-53". NASA National Space Science Data Center. October 8, 2010.
^"KH 8-54". NASA National Space Science Data Center. October 8, 2010.