The KH-11 KENNAN, renamed CRYSTAL in 1982[1] and also referenced by the codenames 1010,[2] and "Key Hole",[2] is a type of reconnaissance satellite launched by the American National Reconnaissance Office since December 1976. Manufactured by Lockheed in Sunnyvale, California, the KH-11 was the first American spy satellite to utilize electro-optical digital imaging, and create a real-time optical observation capability.[3]
Later KH-11 satellites have been referred to by outside observers as KH-11B or KH-12, and by the names "Advanced KENNAN", "Improved Crystal" and "Ikon". The Key Hole series was officially discontinued in favour of a random numbering scheme after repeated public references to KH-8 Gambit, KH-9 Hexagon, and KH-11 satellites.[4] KH-11 satellites are believed to have been the source of some imagery of the Soviet Union and China made public in 1997, as well as images of Sudan and Afghanistan made public in 1998 that were related to the response to the 1998 U.S. embassy bombings.
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It is believed to resemble the Hubble Space Telescope in size and shape, as the satellites were shipped in similar containers. Furthermore, a NASA history of the Hubble,[5] in discussing the reasons for switching from a 3-meter main mirror to a 2.4-meter design, states: "In addition, changing to a 2.4-meter mirror would lessen fabrication costs by using manufacturing technologies developed for military spy satellites." A CIA history states that the primary mirror on the first KH-11s measured 2.34 meters, but sizes increased in later versions.[1] NRO led the development of a computer controlled mirror polishing technique, which was subsequently also used for the polishing of the primary mirror of the Hubble Space Telescope.[6]
Assuming a 2.4-meter mirror, the theoretical ground resolution with no atmospheric degradation and 50% MTF would be roughly 15 cm (6 inches). Operational resolution would be worse due to effects of the atmosphere. Different versions of the KH-11 vary in mass, with earlier blocks ranging from 13,000 to 13,500 kilograms, whilst later blocks have a mass of around 19,600 kg. Its length is believed to be 19.5 meters, and diameter is 3 meters or less.[1][7]
KH-11 was the first reconnaissance satellite equipped with Charge-coupled device (CCD) array technology for imaging. Data is transmitted through a network of communications satellites; the Satellite Data System.[1] The initial ground station for the processing of the electro-optical imaging was a secret National Reconnaissance Office facility in Area 58, located in the continental United States.[8]
Later block satellites may include signals intelligence capabilities and greater sensitivity in broader light spectrums (probably into infrared), as well as an in-flight refueling capability for extended life span and maneuverability.[9]
Later satellites had larger mirrors, with a diameter of around 2.9–3.1 m.[10] Jane's Defence Weekly indicates that the secondary mirror in the Cassegrain reflecting telescope system could be moved, allowing images to be taken from angles unusual for a satellite. Also, there are indications that the satellite can take images every five seconds.
After the failure of the Boeing led Future Imagery Architecture program in 2005, NRO ordered from Lockheed two additional legacy hardware KH-11s. USA-224, the first of these two, was launched in early 2011 two years ahead of schedule, and US $ 2 billion under the initial budget estimate.[11]
Four generations of U.S. electro-optical reconnaissance have been identified:[12][13]
Block I refers to the original KH-11 Kennan satellite, of which five were launched between 19 December 1976 and 17 November 1982.
The three Block II satellites are in the open literature referred to as KH-11B, the alleged DRAGON codename , or Crystal, and are believed to be capable of taking infrared images in addition to optical observations.[14] The first or second Block II satellite was lost in a launch failure.[13]
Four Block III satellites, commonly called KH-12 or Improved Crystal were launched between November 1992 and October 2001. The name "Improved Crystal" refers to the "Improved Metric CRYSTAL System" (IMCS), which adds reference markings for accurate mapping to images obtained by the satellite.[15]
Two electro-optical satellites launched in October 2005 and January 2011 are attributed to Block IV.
The Misty satellite is believed to have been derived from the KH-11, but modified to make it invisible to radar, and hard to detect visually. The first Misty satellite, USA-53, was released by the Space Shuttle Atlantis on mission STS-36. The USA-144 satellite, launched on 22 May 1999 by a Titan IVB from Vandenberg Air Force Base may have been a second Misty satellite,[16] or an Enhanced Imaging System spacecraft. The satellites are sometimes identified as KH-12s.
In 1978, a young CIA employee named William Kampiles was accused of selling a KH-11 System Technical Manual describing design and operation to the Soviets. Kampiles was convicted of espionage and initially sentenced to 40 years in prison.[17] Later, this term was reduced, and after serving 18 years, Kampiles was released in 1996.[18][19]
In 1984 Samuel Loring Morison, an intelligence analyst at the Naval Intelligence Support Center, forwarded three classified images taken by KH-11 to the publication Jane's Fighting Ships. In 1985, Morison was convicted in Federal Court on two counts of espionage and two counts of theft of government property, and was sentenced to two years in prison.[20] He was pardoned by President Clinton in 2001.[21]
Nine KH-11 satellites were launched between 1976 and 1990 aboard Titan-3D and −34D rockets, with one launch failure. For the following five satellite launches between 1992 and 2005, a Titan IV launch vehicle was used. The most recent launch in 2011 was carried out by a Delta IV Heavy rocket. The KH-11 replaced the KH-9 film return satellite, among others, the last of which was lost in a liftoff explosion in 1986.
KH-11 satellites are in either of two standard planes in Sun-synchronous orbits. As shadows help to discern ground features, satellites in a standard plane east of a noon/midnight orbit observe the ground at local afternoon hours, while satellites in a western plane observe the ground at local morning hours.[22][23] Historically launches have therefore been timed to occur either about two hours before or one hour after local noon (or midnight), respectively.[13]
Name | KH-11 Block[23] |
Launch date | ID | NROL number | Orbit | Plane[23] | Orbital decay date |
---|---|---|---|---|---|---|---|
OPS 5705 | 1-1 | 19 December 1976 | 1976-125A | N/A | 247 km x 533 km, i=96.9° | West | 28 January 1979 |
OPS 4515 | 1–2 | 14 June 1978 | 1978-060A | 276 km x 509 km, i=96.8° | West | 23 August 1981 | |
OPS 2581 | 1–3 | 7 February 1980 | 1980-010A | 309 km x 501 km, i=97.1° | East | 30 October 1982 | |
OPS 3984 | 1–4 | 3 September 1981 | 1981-085A | 244 km x 526 km, i=96.9° | West | 23 November 1984 | |
OPS 9627 | 1–5 | 17 November 1982 | 1982-111A | 280 km x 522 km, i=96.9° | East | 13 August 1985 | |
USA-6 | 2-1 | 4 December 1984 | 1984-122A | 335 km x 758 km, i=98°[14] | West | 10 November 1994 | |
Unknown | 2-2 | 28 August 1985 | N/A | Failed to orbit | East | N/A | |
USA-27 | 2–3 | 26 October 1987 | 1987-090A | 300 km x 1000 km, i=98°[14] | East | 11 June 1992 | |
USA-33 | 2–4 | 6 November 1988 | 1988-099A | 300 km x 1000 km, i=98°[14] | West | 12 May 1996 | |
USA-86 | 3-1 | 28 November 1992 | 1992-083A | 408 km x 931 km, i=97.7°[24] | East | 5 June 2000 | |
USA-116 | 3-2 | 5 December 1995 | 1995-066A | 405 km x 834 km, i=97.7°[25] | East | 19 November 2008 | |
USA-129 | 3-3 | 20 December 1996 | 1996-072A | NROL-2 | 292 km x 894 km, i=97.7°[26] | West | |
USA-161 | 4-1 | 5 October 2001 | 2001-044A | NROL-14 | 309 km x 965 km, i=97.9°[27] | East | |
USA-186 | 3–4 | 19 October 2005 | 2005-042A | NROL-20 | 256 km x 1006 km, i=97.9°[28] | West | |
USA-224 | 4-2 | 20 January 2011 | 2011-002A | NROL-49 | 290 km x 985 km, i=97.9°[29] | East |
KH-11 satellites require periodic reboosts to counter atmospheric drag, or to adjust their ground track to surveillance requirements. Based on data collected by amateur observers, the following orbital characteristics of OPS 5705 were calculated by amateur skywatcher Ted Molczan.[30]
OPS 5705 Time period |
Periapsis (AMSL) |
Apoapsis (AMSL) |
Apogee at end of period (AMSL) |
---|---|---|---|
1976 Dec 19 – 23 Dec | 253 km (157 mi) | 541 km (336 mi) | 541 km (336 mi) |
1976 Dec 23 – 1977 Mar 27 | 348 km (216 mi) | 541 km (336 mi) | 537 km (334 mi) |
1977 Mar 27 – 19 Aug | 270 km (170 mi) | 537 km (334 mi) | 476 km (296 mi) |
1977 Aug 19 – 1978 Jan | 270 km (170 mi) | 528 km (328 mi) | 454 km (282 mi) |
1978 Jan – 1979 Jan 28 | 263 km (163 mi) | 534 km (332 mi) | Deorbited |
Unit costs, including launch, in 1990 dollars are estimated to be in the range of US $ 1.25 to 1.75 billion (inflation adjusted US$ 2.1 to 2.94 billion in 2012).[9]
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