Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Naval Ocean Surveillance System

From Wikipedia, the free encyclopedia
(Redirected fromIntruder (satellite))
Series of signals-intelligence satellites of the U.S. Navy
"NOSS" redirects here. For other uses, seeNoss (disambiguation).
"Intruder (satellite)" redirects here. For the program originally rumored to be called Intruder, seeIntegrated Overhead SIGINT Architecture.

A NOSS satellite trio passes the Moon.

TheNaval Ocean Surveillance System (NOSS) is a series ofsignals-intelligencesatellites that have conductedelectronic signals intelligence for theU.S. Navy since the early 1970s.[1] The first series of satellites were codenamed "White Cloud" or "PARCAE", while second- and third-generation satellites have used the codenames "Ranger" and "Intruder".

The system is operated by the United States Navy, and its main purpose wastacticalgeolocation ofSoviet Navy assets during theCold War. NOSS involvessatellite clusters operating inlow Earth orbit to detect radar and other electronic transmissions from ships at sea and locate them using thetime difference of arrival technique.[2]

Satellites

[edit]

First generation NOSS-1 (1976–1987)

[edit]

The first generation of NOSS satellites was developed by theNaval Research Laboratory (NRL) based on the previous generations of electronic listening satellites:Grab (1960–1962) andPoppy (1962–1971). Eight clusters of 3 satellites were launched between 1976 and 1987.[3]

Each launch carried out by anAtlas F,E orH) with a dispenser placed three sub-satellites into orbit. The dispenser is responsible, thanks to itssolid propellant engine, for placing the three sub-satellites into their operational orbit of 1,050 × 1,150km with an inclination of 63°. To be able to track ships, the three satellites maintain a triangular formation with a distance between 30 and 240 km .

Each satellite has on one of its faces a series of antennas intended to collect the signals emitted by ships which are kept constantly turned towards the Earth. The satellite's orientation is maintained bygravity gradient pointed towards the Earth thanks to a boom 10 to 15 meters long.

First generation (Parcae)
NameIDLaunch dateLaunch vehicleLaunch sitePerigeeApogeeInclinationRemarks
OPS 6431 SSU-11976-038C30 April 1976Atlas E/F-MSDVAFB,SLC-3W1,092 km1,128 km63.5°Dispenser designatedOPS 6431 and catalogued as 1976-038A.
OPS 6431 SSU-21976-038D
OPS 6431 SSU-31976-038J
OPS 8781 SSU-11977-112D8 December 1977Atlas E/F-MSDVAFB,SLC-3W1,054 km1,169 km63.4°Dispenser designatedOPS 8781 and catalogued as 1977-112A.
OPS 8781 SSU-21977-112E
OPS 8781 SSU-31977-112F
OPS 7245 SSU-11980-019C3 March 1980Atlas E/F-MSDVAFB,SLC-3W1,035 km1,150 km63.0°Dispenser designatedOPS 7245 and catalogued as 1980-019A.
OPS 7245 SSU-21980-019D
OPS 7245 SSU-31980-019G
OPS 3255 SSU-1N/A9 December 1980Atlas E/F-MSDVAFB,SLC-3WFailed to orbitDispenser designatedOPS 3255, loss of control after engine failure, followed by explosion.
OPS 3255 SSU-2N/A
OPS 3255 SSU-3N/A
OPS 0252 SSU-11983-008E9 February 1983Atlas H-MSDVAFB,SLC-3E1,063 km1,186 km63.40°Dispenser designatedOPS 0252 and catalogued as 1983-008A.
OPS 0252 SSU-21983-008F
OPS 0252 SSU-31983-008H
OPS 6432 SSU-11983-056C9 June 1983Atlas H-MSDVAFB,SLC-3E851 km1,363 km63.4°Dispenser designatedOPS 6432 and catalogued as 1983-056A.
OPS 6432 SSU-21983-056D
OPS 6432 SSU-31983-056G
OPS 8737 SSU-11984-012C5 February 1984Atlas H-MSDVAFB,SLC-3E1,052 km1,172 km63.4°Dispenser designatedOPS 8737 and catalogued as 1984-012A.
OPS 8737 SSU-21984-012D
OPS 8737 SSU-31984-012F
USA-161986-014E9 February 1986Atlas H-MSDVAFB,SLC-3E1,049 km1,166 km63.0°Dispenser designatedUSA-15 and catalogued as 1986-014A.
USA-171986-014F
USA-181986-014H
USA-231987-043E15 May 1987Atlas H-MSDVAFB,SLC-3E1,045 km1,179 km62.9°Dispenser designatedUSA-22 and catalogued as 1987-043A.
USA-241987-043F
USA-261987-043H

Second generation NOSS-2 (1990–1996)

[edit]

The second generation of NOSS satellites, first launched in 1990, adopted the same configuration as the previous generation. The satellites were launched in clusters of three with aTitan Launch Dispenser (TLD) responsible for positioning them in their operational orbit (1,100 × 1,100  km with an inclination of 63.4°) and adopted a triangular configuration.

Four NOSS-2 cluster launches took place between 1990 and 1996 (one failure in 1993).[4][5] The satellites were much heavier and had to be launched by aTitan IV rocket.

The dispenser played a secondary role: after ejecting the NOSS satellites, it placed itself in an elliptical orbit (1,100 × 9,000  km) where a dedicated telecommunications module (Satellite Launch Dispenser Communications System orSLDCOM) was used for tactical military telecommunications.

Second generation
NameIDLaunch dateLaunch vehicleLaunch sitePerigeeApogeeInclinationRemarks
USA-601990-050E8 June 1990Titan IV(405)ACCAFS,LC-411,071 km1,146 km63.4°Dispenser designatedUSA-59 and catalogued as 1990-050A.
USA-611990-050F
USA-621990-050H
USA-741991-076C8 November 1991Titan IV(403)AVAFB,SLC-4E1,052 km1,164 km63.4°Dispenser designatedUSA-72 and catalogued as 1991-076A.
USA-761991-076D
USA-771991-076E
UnnamedN/A2 August 1993Titan IV(403)AVAFB,SLC-4EFailed to orbitExploded due to crack in solid rocket motor caused by poor repair.
UnnamedN/A
UnnamedN/A
USA-1191996-029A12 May 1996Titan IV(403)AVAFB,SLC-4E1,050 km1,166 km63.4°Dispenser designatedUSA-122 and catalogued as 1996-029D.
USA-1201996-029B
USA-1211996-029C

Third generation NOSS-3 (2001–2017)

[edit]
NOSS 3-3 duo passing by Polaris (bright star at the bottom). Movement in this 12.3-seconds exposure is from upper-left to bottom-right; the A object is leading. 6 February 2016, 18:52 (UTC+2),Kyiv.
The NOSS 3-4 duo (2007-027A and C) crossing through thePleiades. Movement in this 10-second exposure is from top to bottom, the A object is leading.

The third generation was deployed after 2001. Unlike previous generations, the satellites are launched and operate in pairs and don't require a dispenser. The combined mass of a satellites pair is 6,500  kg. The orbit is identical to previous generations: 1,100 × 1,100km with an inclination of 64°.

Eight pairs of satellites were launched between 2001 and 2017.[6] The launchers used wereAtlas II,Atlas III andAtlas V.

Third generation (Intruder)
NameIDLaunch dateLaunch vehicleLaunch siteNROL designationPerigeeApogeeInclinationRemarks
USA-1602001-040A8 September 2001Atlas IIASVAFB,SLC-3ENROL-131,100 km1,100 km63.0°
Unnamed*2001-040C
USA-1732003-054A2 December 2003Atlas IIASVAFB,SLC-3ENROL-181,013 km1,200 km63.4°
Unnamed*2003-054C
USA-1812005-004A3 February 2005Atlas IIIBCCAFS,SLC-36BNROL-231,011 km1,209 km63.4°
Unnamed*2005-004C
USA-1942007-027A15 June 2007Atlas V 401CCAFS,SLC-41NROL-301,053 km1,163 km63.4°Launched into lower orbit than planned, spacecraft corrected under own power, at expense of operational life.
Unnamed*2007-027C
USA-2292011-014A15 April 2011Atlas V 411VAFB,SLC-3ENROL-341,015 km1,207 km63.46°
Unnamed*2011-014B
USA-2382012-048A13 September 2012Atlas V 401VAFB,SLC-3ENROL-361,056 km1,158 km63.4°
Unnamed*2012-048P
USA-2642015-058A8 October 2015Atlas V 401VAFB,SLC-3ENROL-551,013 km1,201 km63.4°
Unnamed*2015-058R
USA-2742017-011A1 March 2017Atlas V 401VAFB,SLC-3ENROL-791,010 km1,204 km63.4°
Unnamed*2017-011B
Note: * One satellite from each third generation pair is officially catalogued as debris.[1][2]

Fourth generation NOSS-4 (2022–)

[edit]
Fourth generation (Intruder F/O)
NameIDLaunch dateLaunch vehicleLaunch siteNROL designationPerigeeApogeeInclinationRemarks
USA-3272022-040A17 April 2022Falcon 9 Block 5VAFB,SLC-4ENROL-85[7]1,100 km1,100 km63.4°Launched.
USA-49824 March 2025Falcon 9 Block 5CCAFS,SLC-40NROL-691,100 km1,100 km63.4°Launched.

Cost

[edit]

The costs of the NOSS satellites (excluding costs for the launch vehicle), which were destroyed in a Titan IV launch failure in 1993, were US$800 million (inflation adjusted US$ 1.7 billion in 2024).[8]

See also

[edit]

References

[edit]
  1. ^"Display: SSU 1/2 1976-038C". NASA. 14 May 2020. Retrieved29 October 2020.Public Domain This article incorporates text from this source, which is in thepublic domain.
  2. ^"NOSS Double and Triple Satellite Formations".satobs.org.
  3. ^"Parcae (NOSS-1, White Cloud)".Gunter's Space Page. Retrieved20 June 2025.
  4. ^"Parcae 10, 11, 12, 13 (improved Parcae / NOSS-2 1, 2, 3, 4)".Gunter's Space Page. Retrieved20 June 2025.
  5. ^"SLDCOM (TLD)".Gunter's Space Page. Retrieved20 June 2025.
  6. ^"Intruder 1, ..., 18 (NOSS-3 1, ..., 9)".Gunter's Space Page. Retrieved20 June 2025.
  7. ^Krebs, Gunter (2 December 2021)."Intruder F/O 1, 2 (NOSS-4 1, 2) ?".Gunter's Space Page. Retrieved16 March 2022.
  8. ^Weiner, Tim (4 August 1993)."Titan Lost Payload: Spy-Satellite System Worth $800 Million".The New York Times.

External links

[edit]
Current programs
Facilities & commands
Technology & Science
Satellite lines & projects
People
History
Past programs
Founders
IMINT
Photographic
Electro-optical
Synthetic-aperture radar
SIGINT
Low Earth orbit
Highly elliptical orbit
Geosynchronous Earth orbit
MASINT
Primary mission
Secondary mission
R&D
Primary mission
Unknown
USA number
Retrieved from "https://en.wikipedia.org/w/index.php?title=Naval_Ocean_Surveillance_System&oldid=1311482256"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp