KH-9 (BYEMAN codename HEXAGON), commonly known as Big Bird or Keyhole-9, 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, all but one were successful. Photographic film aboard the KH-9 was sent back to Earth in recoverable film return capsules for processing and interpretation. The best ground resolution achieved by the main cameras was better than 0.6 metres (2 ft 0 in).
The KH-9 was declassified in September 2011 and an example was put on public display for a single day on September 17, 2011 in the parking lot of the Steven F. Udvar-Hazy Center of the National Air and Space Museum.
The KH-9 was originally 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. 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) was completed in May 1971, and it was subsequently shipped to Vandenberg Air Force Base in a 70-foot (21 m) container. Ultimately, four generations ("blocks") of KH-9 Hexagon reconnaissance satellites were developed. KH9-7 (1207) was the first to fly a Block-II panoramic camera and SBA. Block-III (vehicles 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 was equipped with an extended command system using plated wire memory. In the mid 1970s, over 1,000 people in the Danbury, Connecticut area worked on the secret project.
A reentry vehicle from the first Hexagon satellite sank to 16,000 feet (4,900 m) below the Pacific Ocean after its parachute failed. The USS Trieste II (DSV-1) retrieved its payload in April 1972 after a lengthy search but the film disintegrated due to the nine months underwater, leaving no usable photographs.
Over the duration of the program the lifetime of the individual satellites increased steadily. The final KH-9 operated for up to 275 days. Different versions of the satellite varied in mass; most weighed 25,100 or 29,300 pounds (11,400 or 13,300 kg).
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 ten feet (3.0 m) (compared to five feet (1.5 m) for the Agena) and a length of six feet (1.8 m). It incorporated a secondary propulsion system inherited from the Agena. SCS was equipped with deployable solar arrays and an unfurlable parabolic antenna for high data rate communication.
The main camera system was designed by Perkin-Elmer to take stereo images, 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 90–200 miles (480,000–1,060,000 ft; 140–320 km). The camera optical layout is an f/3.0 folded Wright Camera, with a focal length of 60 in (1.5 m). The system aperture is defined by a 20 in (0.51 m) 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-degree-angle flat mirror, which reflects the light to a 36-inch-diameter (0.91 m) 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 degrees wide, and achieved a ground resolution better than 2 ft (0.61 m) during the later phase of the project.
Missions 1205 to 1216 carried a "mapping camera" (also known as a "frame camera") that used 9 inch film and had a moderately low resolution of initially 30 ft (9 m), which improved to 20 ft (6 m) on later missions (somewhat better than LANDSAT). Intended for mapmaking, photos this camera took cover essentially the entire Earth with at least some images between 1973 and 1980. Almost all the imagery from this camera, amounting to 29,000 images, each covering 1,300 square miles (3,400 km2), was declassified in 2002 as a result of Executive order 12951, 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.
High-altitude atmospheric density
Missions 1205 to 1207 carried Doppler beacons to help map the atmospheric density at high altitudes in an effort to understand the effect on ephemeris predictions. The measurements of the atmospheric density were released through NASA.
Missions 1203, 1207, 1208, 1209, and 1212 to 1219 included Ferret ELINT subsatellites, 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.
|Name||Block||Mission no.||Launch date||NSSDC ID
|Other Name||Launch vehicle||Orbit||Decay date|
|KH9-1||I||1201||1971 June 15||1971-056A
|OPS 7809||Titan IIID||184.0 km × 300.0 km, i=96.4°||1971 Aug 06|
|KH9-2||I||1202||1972 Jan 20||1972-002A
|OPS 1737||Titan IIID||157.0 km × 331.0 km, i=97.0°||1972 Feb 29|
|KH9-3||I||1203||1972 Jul 7||1972-052A
|OPS 7293||Titan IIID||174.0 km × 251.0 km, i=96.9°||1972 Sep 13|
|KH9-4||I||1204||1972 Oct 10||1972-079A
|OPS 8314||Titan IIID||160.0 km × 281.0 km, i=96.5°||1973 Jan 08|
|KH9-5||I||1205||1973 Mar 9||1973-014A
|OPS 8410||Titan IIID||152.0 km × 270.0 km, i=95.7°||1973 May 19|
|KH9-6||I||1206||1973 Jul 13||1973-046A
|OPS 8261||Titan IIID||156.0 km × 269.0 km, i=96.2°||1973 Oct 12|
|KH9-7||II||1207||1973 Nov 10||1973-088A
|OPS 6630||Titan IIID||159.0 km × 275.0 km, i=96.9°||1974 Mar 13|
|KH9-8||II||1208||1974 Apr 10||1974-020A
|OPS 6245||Titan IIID||153.0 km × 285.0 km, i=94.5°||1974 Jul 28|
|KH9-9||II||1209||1974 Oct 29||1974-085A
|OPS 7122||Titan IIID||162.0 km × 271.0 km, i=96.7°||1975 Mar 19|
|KH9-10||II||1210||1975 Jun 8||1975-051A
|OPS 6381||Titan IIID||157.0 km × 234.0 km, i=96.3°||1975 Nov 05|
|KH9-11||II||1211||1975 Dec 4||1975-114A
|OPS 4428||Titan IIID||157.0 km × 234.0 km, i=96.7°||1976 Apr 01|
|KH9-12||II||1212||1976 Jul 8||1976-065A
|OPS 4699||Titan IIID||159.0 km × 242.0 km, i=97.0°||1976 Dec 13|
|KH9-13||III||1213||1977 Jun 27||1977-056A
|OPS 4800||Titan IIID||155.0 km × 239.0 km, i=97.0°||1977 Dec 23|
|KH9-14||III||1214||1978 Mar 16||1978-029A
|OPS 0460||Titan IIID||172.0 km × 218.0 km, i=96.4°||1978 Sep 11|
|KH9-15||III||1215||1979 Mar 16||1979-025A
|OPS 3854||Titan IIID||177.0 km × 256.0 km, i=96.3°||1979 Sep 22|
|KH9-16||III||1216||1980 Jun 18||1980-052A
|OPS 3123||Titan IIID||169.0 km × 265.0 km, i=96.5°||1981 Mar 06|
|KH9-17||III||1217||1982 May 11||1982-041A
|OPS 5642||Titan IIID||177.0 km × 262.0 km, i=96.4°||1982 Dec 05|
|KH9-18||III||1218||1983 Jun 20||1983-060A
|OPS 0721||Titan 34D||163.0 km × 224.0 km, i=96.4°||1984 Mar 21|
|KH9-19||IV||1219||1984 Jun 25||1984-065A
|USA 2||Titan 34D||170.0 km × 230.0 km, i=96.5°||1984 Oct 18|
|KH9-20||IV||1220||1986 Apr 18||1986-F03||launch failed||Titan 34D||—||—|
(NSSDC ID Numbers: See COSPAR)
The total cost of the 20 flight KH-9 program from FY1966 to FY1986 was US$3.262 billion in respective year dollars (equivalent to 14.36 billion in 2018, with an average reference year of 1976).
Data source: The Encyclopedia of US Spacecraft and NSSDC
- Launch vehicle: Titan IIID/34D
- Total weight: 11,400 kg (25,100 lb), with mapping camera 13,300 kg (29,300 lb)
- Reentry weight: 5,330 kg (11,750 lb)
- Max. diameter (main body): 3.05 m (120 in)
- Length (with mapping camera): 16.21 m (638 in)
- Orbit: elliptical, 100 miles by 150 miles
- Scanners: television, radio, and high resolution camera
Other U.S. imaging spy satellites:
- Corona series:
- KH-5 ARGON
- KH-6 LANYARD
- KH-7 and KH-8 GAMBIT
- Manned Orbiting Laboratory (KH-10)
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