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Satellite Data System

From Wikipedia, the free encyclopedia
American military satellite communication system

The current SDS-3 constellation, consisting of threeMolniya orbit type and two geostationary satellites

TheSatellite Data System (SDS) is a system of United Statesmilitary communications satellites. At least three generations have been used:SDS-1 from 1976 to 1987;SDS-2 from 1989 to 1996;SDS-3 from 1998 to the present. It is believed that these satellites were known by the code nameQuasar.[1] The first generation was named simply 'SDS', the second generation was named 'Quasar' and the third generation each had their own designations.[2]

Orbital characteristics

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SDS satellites have ahighly elliptical orbit, going from about 300 kilometers atperigee to roughly 39,000 km atapogee in order to allow communications withpolar stations that cannot contactgeosynchronous satellites. The high apogee meant that the polar regions were visible for long amounts of time, and only two satellites were required in order to achieve constant communications ability. In addition, two geostationary satellites appear to be part of the system. The SDS satellites were constructed byHughes Aircraft Company.

Mission

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The primary purpose of the SDS satellites is to relay imagery from low-flyingreconnaissance satellites, notably theKeyhole optical reconnaissance andLacrosse/Onyx radar reconnaissance satellites to ground stations in theUnited States.[3]

SDS-1

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Releasable Picture of NRO satellite, possible SDS-1
The SDS 3-4 satellite (USA 179, 2004-034A) created a tiny trail perpendicular to the star trails in this 10 second exposure with a Zeiss Sonnar MC 2.8/180mm lens made by amateur satellite observer Marco Langbroek.

Each SDS-1 satellite had 12 channels available forUltra high frequency (UHF) communication. They werecylindrical in shape, roughly 25 ft (7.6 m) long. 980watts of electrical power were available fromsolar panels andbatteries. The SDS-1 had a mass of 630 kg (1,390 lb) and was launched onTitan-3B rockets. The SDS-1 satellites had similar orbits to the Air Force'sJumpseatELINT satellites.[4]

It has been speculated that the early satellites served as data relays for the firstKH-11 Kennen reconnaissance satellites.[5]

SDS-2

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The SDS-2 is significantly more massive at 2,335 kg (5,148 lb), with three separate communication dishes, including one for aK-band downlink. Two dishes are 4.5 m (15 ft) in diameter, while the third is 2 m (6 ft 7 in) in diameter. The solar arrays generate 1238 watts of power. It is believed that theSpace Shuttle has been used to launch several satellites, possibly on missionsSTS-28,STS-38, andSTS-53. Other launches have used theTitan IVlaunch vehicle.

Satellites

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NameCOSPAR ID[6]
SATCAT №
Launch dateLaunch vehicleLaunch siteLaunch designationPerigeeApogeeInclinationRemarks

First generation

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OPS 78371976-050A
08871
2 June 1976Titan III(34)BVAFB,SLC-4WSDS F-1380 km39315 km63.3 deg
OPS 79401976-080A
09270
6 August 1976Titan III(34)BVAFB,SLC-4WSDS F-2380 km39315 km63.3 deg
OPS 73101978-075A
10993
5 August 1978Titan III(34)BVAFB,SLC-4WSDS F-3380 km39315 km63.3 deg
OPS 58051980-100A
12093
13 December 1980Titan III(34)BVAFB,SLC-4W
USA-41984-091A
15226
28 August 1984Titan III(34)BVAFB,SLC-4WSDS F-5A
USA-9195-014A
15546
8 February 1985Titan III(34)BVAFB,SLC-4WUSA-9
USA-211987-015A
17506
15 February 1987Titan III(34)BVAFB,SLC-4WSDS F-6

Second generation

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USA-401989-061B
20167
2 June 1989Space Shuttle Columbia
STS-28/Orbus-21S
KSC,LC-39BN/A
USA-671990-097B
20963
15 November 1990Space Shuttle Atlantis
STS-38/Orbus-21S
KSC,LC-39AGeosynchronous satellite, deployed along withProwler and initially misidentified as aMagnum SIGINT spacecraft
USA-891992-086B
22518
2 December 1992Space Shuttle Discovery
STS-53/Orbus-21S
KSC,LC-39A
USA-1251996-038A
23945
3 July 1996Titan IV(405)ACCAFS,LC-40

Third generation

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USA-1371998-005A
25148
29 January 1998Atlas IIACCAFS,SLC-36ANROL-5Capricorn,Molniya orbit
USA-1552000-080A
26635
6 December 2000Atlas IIASCCAFS,SLC-36ANROL-10Great Bear, geosynchronous satellite at 10° West
USA-1622001-046A
26948
11 October 2001Atlas IIASCCAFS,SLC-36BNROL-12Aquila, geosynchronous satellite at 144° West
USA-1792004-034A
28384
31 August 2004Atlas IIASCCAFS,SLC-36ANROL-1Nemesis,Molniya orbit, final Atlas II launch
USA-1982007-060A
32378
10 December 2007Atlas V 401CCAFS,SLC-41NROL-24Scorpius,Molniya orbit
USA-2272011-011A
37377
11 March 2011Delta IV-M+(4,2)CCAFS,SLC-37BNROL-27Gryphon, geosynchronous satellite at 10° West, replaced USA-155
USA-2362012-033A
38466
20 June 2012Atlas V 401CCAFS,SLC-41NROL-38Drake, geosynchronous satellite at 144° West, replacement for USA-162
USA-2522014-027A
39751
22 May 2014Atlas V 401CCAFS,SLC-41NROL-33Geosynchronous satellite
USA-2692016-047A
41724
28 July 2016Atlas V 421CCAFSSLC-41NROL-61Spike,Geosynchronous orbit, might be a new generation[7]
USA-2792017-066A
42973
15 October 2017Atlas V 421CCAFS,SLC-41NROL-52LikelyGeosynchronous orbit[8]

References

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  1. ^Jonathan's Space Report:NRO Satellite Names
  2. ^Jonathan's Space Report:Satellite Catalogue
  3. ^Richelson, J.T. (2001).The Wizards of Langley. Inside the CIA's Directorate of Science and Technology. Boulder, Colorado: Westview Press.ISBN 9780813340593.
  4. ^National Reconnaissance Office: "NRO Brochure circa 1997"[permanent dead link]
  5. ^Day, Dwayne A. (26 February 2018)."Shadow dancing: the Satellite Data System". The Space Review.
  6. ^Jonathan's Space Report:List of satellite launches
  7. ^"NROL-61 satellite launched Thursday spotted in space by sky-watchers". Spaceflight Now. 30 July 2016.
  8. ^Graham, William (15 October 2017)."Atlas V finally launches with NROL-52". NASASpaceFlight.com. Retrieved15 October 2017.
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