KH-9 Hexagon

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File:KH-9 HEXAGON.jpg
A KH-9 HEXAGON main features

KH-9 (BYEMAN codename HEXAGON), commonly known as Big Bird or KeyHole-9,[1] was a series of photographic reconnaissance satellites launched by the United States between 1971 and 1986. Of twenty launch attempts by the National Reconnaissance Office (NRO), all but one were successful.[2] Photographic film aboard the KH-9 was stored on RCA Astro Electronic Division take up reel system then sent back to Earth in recoverable film return capsules for processing and interpretation. The highest ground resolution achieved by the main cameras of the satellite was Template:Cvt,[3] though another source says "images in the "better-than-one-foot" category" for the last "Gambit" missions.[4]

They are also officially known as the Broad Coverage Photo Reconnaissance satellites (Code 467), built by Lockheed Corporation for the NRO.[1]

The satellites were an important factor in determining Soviet military capabilities and in the acquisition of accurate intelligence for the formulation of U.S. national policy decisions as well as deployment of U.S. forces and weapon systems. The satellites were instrumental in U.S. National Technical Means of Verification of Strategic Arms Limitation Talks (SALT) and the Anti-Ballistic Missile Treaty (ABMT).[5]

The KH-9 was declassified in September 2011 and an example was put on public display for a single day on 17 September 2011 in the parking lot of the Steven F. Udvar-Hazy Center of the National Air and Space Museum.[6][7][8]

On 26 January 2012, the National Museum of the United States Air Force put a KH-9 on public display along with its predecessors the KH-7 and KH-8.[9]

Development

KH-9 was, according to many who worked on it, the most sophisticated mechanical satellite in history.Template:R It was conceived in the early 1960s as a replacement for the CORONA search satellites. The goal was to search large areas of the Earth with a medium resolution camera. The KH-9 carried two main cameras, although a mapping camera was also carried on several missions. The photographic film from the cameras was sent to recoverable re-entry vehicles and returned to Earth, where the capsules were caught in mid-air by an aircraft. Four re-entry vehicles were carried on most missions, with a fifth added for missions that included a mapping camera.

Between September 1966 and July 1967, the contractors for the Hexagon subsystems were selected. Lockheed Missiles and Space Company (LMSC) was awarded the contract for the Satellite Basic Assembly (SBA), Perkin Elmer for the primary Sensor Subsystem (SS), McDonnell for the Reentry Vehicle (RV), RCA Astro-Electronics Division for the Film Take-Up system, and Itek for the Stellar Index camera (SI). Integration and ground-testing of Satellite Vehicle-1 (SV-1) were completed in May 1971, and it was subsequently shipped to Vandenberg Air Force Base in a Template:Cvt container. Ultimately, four generations ("blocks") of KH-9 HEXAGON reconnaissance satellites were developed. KH9-7 (missions 7 to 12) was the first to fly a Block-II panoramic camera and SBA. Block-III (missions 13 to 18) included upgrades to electrical distribution and batteries. Two added tanks with ullage control for the Orbit Adjust System (OAS) and new thrusters for the Reaction Control System (RCS) served to increase KH-9's operational lifetime. In addition, the nitrogen supply for the film transport system and the camera vessel was increased. Block-IV (missions 19 and 20) was equipped with an extended command system using plated-wire memory.[10] In the mid 1970s, over 1,000 people in the Danbury, Connecticut area worked on the secret project.[11]

A reentry vehicle from the first Hexagon satellite sank to Template:Cvt below the Pacific Ocean after its parachute failed. The Script error: No such module "WPSHIPS utilities". retrieved its payload in April 1972 after a lengthy search, but the film had disintegrated during the nine months underwater, leaving no usable photographs.[12]

Over the duration of the program, the lifetime of the individual satellites increased steadily. The final KH-9 operated for 275 days. The satellite mass with and without the Mapping Camera System was Template:Cvt, respectively.

NRO intended to replace HEXAGON with ZEUS, later DAMON—HEXAGON's camera flown on the Space Shuttle—but DAMON was canceled in December 1980.Template:R[13] In December 1976 NRO launched the first KH-11 KENNEN. While its electro-optical digital imaging had a smaller field of view than HEXAGON, by not needing film KENNEN was usable for years.Template:R

Main KH-9 components

Satellite Control Section

File:HexagonSatelliteControlSection.png
Satellite Control Section

The Satellite Control Section (SCS), which forms the aft part of the SBA, started as Air Force Project 467. SCS was intended as a more capable replacement for the on-orbit propulsion, which had been provided by the Agena upper stage for previous generations of reconnaissance satellites. The SCS featured an increased diameter of Template:Cvt (compared to Template:Cvt for the Agena) and a length of Template:Cvt. It housed hydrazine propellant tanks for the pressure fed Orbital Adjust System (OAS) and the Reaction Control System (RCS). OAS and RCS were connected by a transfer line to facilitate propellant exchange. The tank pressure was maintained within the operational range by additional high pressure nitrogen tanks. The SCS incorporated a freon gas system for backup attitude control inherited from the Agena, commonly referred to as "lifeboat".[14] SCS was equipped with deployable solar panels and an unfurlable parabolic antenna for high data rate communication.[15]

Main camera

File:HEXAGON MainCameraOpticalPath.png
A main camera optical path
File:KH9 resolution maincamera.png
A achieved ground resolution of Satellite Vehicles (SV) 1 to 18 main cameras.
File:Kubinka3.jpg
A KH-9 image of the Soviet civil Moscow Domodedovo Airport misidentified in the original document as Kubinka airfield

The main camera system was designed by Perkin-Elmer to take stereo images,[16] with a forward looking camera on the port side, and an aft looking camera on the starboard side. Images were taken at altitudes ranging from Template:Cvt. The camera optical layout is an f/3.0 folded Wright camera, with a focal length of Template:Cvt. The system aperture is defined by a Template:Cvt diameter aspheric corrector plate, which corrects the spherical aberration of the Wright design. In each of the cameras the ground image passes through the corrector plate to a 45°-angle flat mirror, which reflects the light to a Template:Cvt-diameter concave main mirror. The main mirror directs the light through an opening in the flat mirror and through a four-element lens system onto the film platen. The cameras could scan contiguous areas up to 120° wide, and achieved a ground resolution better than Template:Cvt during the later phase of the project.[3][17] Dwayne Allen Day calculated, using disclosed specifications, that HEXAGON was capable of Template:Cvt at nadir, and Template:Cvt at apogee.[18]

Mapping camera

Missions 1205 to 1216 carried a "mapping camera" (also known as a "frame camera") that used Template:Cvt film and had a moderately low resolution of initially Template:Cvt, which improved to Template:Cvt on later missions [19] (somewhat better than LANDSAT). Intended for mapmaking, photos this camera took cover the entire Earth with images between 1973 and 1981.[20] Almost all the imagery from this camera, amounting to 29,000 images, each covering Template:Cvt, was declassified in 2002 as a result of Executive order 12951,[21] the same order which declassified CORONA, and copies of the films were transferred to the U.S. Geological Survey's Earth Resources Observation Systems office.[22]

Scientific analysis of declassified KH-9 satellite images continues to reveal historic trends and changes in climate and terrestrial geology. A 2019 study of glacial melt in the Himalayas over the past half-century used data collected by KH-9 satellites throughout the 1970s and 1980s to demonstrate that melt rates had doubled since 1975.[23]

The KH-9 was never a backup project for the KH-10 Manned Orbital Laboratory. It was developed solely as a replacement for the Corona search system.[14]

Reentry vehicles

The forward section of KH-9 housed four McDonnell Douglas Mark 8 satellite reentry vehicles (RV), which were fed film exposed by the main cameras. Each RV had an empty mass of 434 kg. It housed a film take-up assembly (built by RCA Astro Electronic Division) with a mass of 108 kg, and could store about 227 kg of film. The twelve mapping missions were equipped with an additional General Electrics Mark V RV, which could store about 32 kg of film for a total mass of 177 kg.[14]

High-altitude atmospheric density

Missions 1205 to 1207 carried Doppler beacons[24] to help map the atmospheric density at high altitudes in an effort to understand the effect on ephemeris predictions.[25][26] The measurements of the atmospheric density were released through NASA.[27]

ELINT subsatellites

Stereo pair of KH-9 imagery (Los Angeles-1968/06)
Stereo pair of KH-9 imagery (Los Angeles-1968/06)

Missions 1203, 1207, 1208, 1209, and 1212 to 1219 included Ferret ELINT sub-satellites, which were launched into a high Earth orbit to catalogue Soviet air defence radars, eavesdrop on voice communications, and tape missile and satellite telemetry. Missions 1210 to 1212 also included scientific subsatellites.[28][29][30][31][32][33][34][35][36]

IRCB (S73-7)

IRCB (Infra-Red Calibration Balloon) was an 66 cm diameter inflatable calibration sphere orbited in the Space Test Program. It was a piggy-back payload on KH9-8 (1208) boosting it to a 500 mile (800 kilometers) circular orbit. It disappeared from ground-based sensors in the 1990s, and was found again in 2024.[37][38]

KH-9 missions

Name Block [10] Mission no. Launch date NSSDC ID
NORAD #
Other Name Launch vehicle Orbit Decay date
KH9-1 I 1201 15 June 1971 1971-056A [39]
05297
OPS 7809 Titan IIID 184.0 km × 300.0 km, i=96.4° 6 August 1971 [39]
KH9-2 I 1202 20 January 1972 1972-002A [40]
05769
OPS 1737 Titan IIID 157.0 km × 331.0 km, i=97.0° 29 February 1972 [40]
KH9-3 I 1203 7 July 1972 1972-052A [41]
06094
OPS 7293 Titan IIID 174.0 km × 251.0 km, i=96.9° 13 September 1972 [41]
KH9-4 I 1204 10 October 1972 1972-079A [42]
06227
OPS 8314 Titan IIID 160.0 km × 281.0 km, i=96.5° 8 January 1973 [42]
KH9-5 I 1205 9 March 1973 1973-014A [43]
06382
OPS 8410 Titan IIID 152.0 km × 270.0 km, i=95.7° 19 May 1973 [43]
KH9-6 I 1206 13 July 1973 1973-046A [44]
06727
OPS 8261 Titan IIID 156.0 km × 269.0 km, i=96.2° 12 October 1973 [44]
KH9-7 II 1207 10 November 1973 1973-088A [45]
06928
OPS 6630 Titan IIID 159.0 km × 275.0 km, i=96.9° 13 March 1974 [45]
KH9-8 II 1208 10 April 1974 1974-020A [46]
07242
OPS 6245 Titan IIID 153.0 km × 285.0 km, i=94.5° 28 July 1974 [46]
KH9-9 II 1209 29 October 1974 1974-085A [47]
07495
OPS 7122 Titan IIID 162.0 km × 271.0 km, i=96.7° 19 March 1975 [47]
KH9-10 II 1210 8 June 1975 1975-051A [48]
07918
OPS 6381 Titan IIID 157.0 km × 234.0 km, i=96.3° 5 November 1975 [48]
KH9-11 II 1211 4 December 1975 1975-114A [49]
08467
OPS 4428 Titan IIID 157.0 km × 234.0 km, i=96.7° 1 April 1976 [49]
KH9-12 II 1212 8 July 1976 1976-065A [50]
09006
OPS 4699 Titan IIID 159.0 km × 242.0 km, i=97.0° 13 December 1976 [50]
KH9-13 III 1213 27 June 1977 1977-056A [51]
10111
OPS 4800 Titan IIID 155.0 km × 239.0 km, i=97.0° 23 December 1977 [51]
KH9-14 III 1214 16 March 1978 1978-029A [52]
10733
OPS 0460 Titan IIID 172.0 km × 218.0 km, i=96.4° 11 September 1978 [52]
KH9-15 III 1215 16 March 1979 1979-025A [53]
11305
OPS 3854 Titan IIID 177.0 km × 256.0 km, i=96.3° 22 September 1979 [53]
KH9-16 III 1216 18 June 1980 1980-052A [54]
11850
OPS 3123 Titan IIID 169.0 km × 265.0 km, i=96.5° 6 March 1981 [54]
KH9-17 III 1217 11 May 1982 1982-041A [55]
13170
OPS 5642 Titan IIID 177.0 km × 262.0 km, i=96.4° 5 December 1982 [55]
KH9-18 III 1218 20 June 1983 1983-060A [56]
14137
OPS 0721 Titan 34D 163.0 km × 224.0 km, i=96.4° 21 March 1984 [56]
KH9-19 IV 1219 25 June 1984 1984-065A [57]
15063
USA 2 Titan 34D 170.0 km × 230.0 km, i=96.5° 18 October 1984 [57]
KH9-20 IV 1220 18 April 1986 1986-F03 Launch failed [2] Titan 34D

(NSSDC ID Numbers: See COSPAR)

Cost

The total cost of the 20 flights KH-9 program from FY1966 to FY1986 was US$3.262 billion in respective year dollars (equivalent to Expression error: Unrecognized punctuation character "[". billion in Template:Inflation-year, with an average reference year of 1976).[10]

Specifications

Data source: The Encyclopedia of US Spacecraft [1] and NSSDC

Declassification

The HEXAGON images have been declassified in 2011 as a continuation of Executive Order 12951. [59][60] The declassified imagery has since been used to conduct Earth observation (EO) by numerous scholars, offering insight into past cultures and climate research. The imagery has been utilized by a team of scientists from Dartmouth College to detect Roman forts in Syria, [61] the Catalan Institute of Classical Archaeology (ICAC) to detect qanat irrigation systems, [62] a team of scientists from Newcastle University to detect desertification and record qanat systems in Skoura Oasis, Morocco[63] and to record qanat systems in Kharga Oasis, Egypt,[64] and a multidisciplinary team of scientists from Italy's Institute of Atmospheric Sciences and Climate (ISAC), Natural Research Council (CNR), Newcastle University, The University of Al-Qadisiyah, and the Italian Space Agency (ASI) to map archaeological sites and ancient irrigation systems and study the climate-water-agriculture-heritage nexus in Southern Iraq.[65]

Gallery

See also

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Other U.S. imaging spy satellites:

References

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  1. a b c Script error: No such module "citation/CS1". p.32 Big Bird
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  8. Doyle, John M., Big Bird, uncaged, Air and Space, December 2011/January 2012, p.10
  9. Cohen, Aubrey, "Three former spy satellites go on display" Seattle Post-Intelligencer 26 January 2012
  10. a b c Script error: No such module "citation/CS1". Template:PD-notice
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  16. Doyle, John M., Big Bird, uncaged, Air & Space, December 2011/January 2012, p.10
  17. Script error: No such module "citation/CS1". Template:PD-notice
  18. Script error: No such module "citation/CS1".
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  20. NARA ARC database description of "Keyhole-9 (KH-9) Satellite Imagery", accession number NN3-263-02-011
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  57. a b Script error: No such module "citation/CS1". Template:PD-notice
  58. a b c Script error: No such module "citation/CS1". Template:PD-notice
  59. Executive Order 12951
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External links

Template:Sister project

Template:National Reconnaissance Office Script error: No such module "Navbox". Template:US Reconnaissance Satellites