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Milstar

Milstar
Artist's impression of a Milstar Block I spacecraft
Manufacturer Lockheed Martin (prime)
TRW
Boeing (formerly Hughes)
Country of origin United States
Operator U.S. Air Force
Applications Military communications
Specifications
Bus Milstar Block I
Milstar Block II
Design life 10 years
Launch mass 4,500 kilograms (9,900 lb)
Regime Geosynchronous
Production
Status Out of production
Active
Built 6
Launched 6
Operational 5
Lost 1
First launch USA-99, 1994-02-07
Last launch USA-169, 2003-04-08

Milstar, originally meaning Military Strategic and Tactical Relay, is a constellation of military communications satellites in geostationary orbit, which are operated by the United States Air Force, and provide secure and jam-resistant worldwide communications to meet the requirements of the Armed Forces of the United States. Six spacecraft were launched between 1994 and 2003, of which five are operational, and the sixth was lost in a launch failure.

Contents

  • History 1
  • Characteristics 2
    • Spacecraft 2.1
  • See also 3
  • External links 4

History

The first Milstar satellite was launched on 7 February 1994 aboard the first Titan IV(401)A rocket. It was followed by a second spacecraft on 7 November 1995. The first two satellites were Block I spacecraft, or Milstar DFS-1 and 2.

The four later satellites were Block II spacecraft, which featured an additional medium data-rate payload. The first Block II satellite (DFS-3m, a hybrid mix of largely Block I support systems and LDR payload and a MDR (Medium Data Rate) Block II payload) was launched on 30 April 1999, using a Titan IV(401)B rocket. Due to a database error affecting the attitude control system of the Centaur upper stage of its carrier rocket, it was placed into a lower orbit than had been planned, and damaged by deployment at excessive rates. It could not be raised into its operational orbit due to fuel limitations. Its orbit was raised as much as possible to increase the expected lifetime and then it was permanently turned off after 10 days. It was the third consecutive, and last, failure of a Titan IV rocket. The remaining three satellites (DFS-4, -5, and -6) were launched on 27 February 2001, 15 January 2002, and 8 April 2003.

The Milstar system consists of three segments; the space segment which consists of the five satellites, ground terminals and users, and stations to command and control the satellites. The Military Satellite Communications Systems Wing (MCSW) division of the United States Air Force Space Command Space and Missile Systems Center, located at Los Angeles AFB was responsible for development and acquisition of the Milstar space and mission control segments. The Electronic Systems Center at Hanscom AFB is responsible for the US Air Force portion of the terminal segment development and acquisition. The 4th Space Operations Squadron at Schriever AFB and the 148th Space Operations Squadron at Vandenberg AFB are responsible for providing real-time satellite control and communications payload management.

In August 2010 control of the Milstar system was transferred to the Advanced Extremely High Frequency program, in preparation for the launch of the first AEHF satellite, USA-214. Advanced Extremely High Frequency satellites are intended to replace Milstar.

Characteristics

Milstar satellites provide secure, jam resistant, worldwide communications to meet the requirements of the United States military. They were built by Lockheed Martin Missiles and Space Corporation, at a cost of US$800 million each. Each satellite has a design life of 10 years. Six were built, of which five reached their operational geostationary orbits, and remain in service. Launches were made using Titan IV rockets with Centaur upper stages, and all six occurred from Space Launch Complex 40 at the Cape Canaveral Air Force Station. The satellites are designed to provide communications which are hard to detect and intercept, and to be survivable in the event of nuclear warfare.

The spacecraft have a mass of 4,500 kilograms (9,900 lb), and are equipped with solar panels which generate eight kilowatts of electric power to power its transponders. Both Block I and Block II satellites provide low data-rate communications at bandwidths between 75 bit/s and 2,400 bit/s, whilst the Block II spacecraft can also provide medium data-rate communications between 4.8 kbit/s and 1.544 Mbit/s. The satellites' uplinks operate in the Q band, while their downlinks operate within the Ka band. The uplink corresponds to the extremely high frequency band while downlink corresponds to the super high frequency radio band.

Each Milstar satellite serves as a switchboard to direct traffic between terminals on the Earth. The satellites process the signals transmitted to them, and can link with other Milstar satellites through crosslinks, to reduce the requirement for ground-controlled switching. The spacecraft are used for encrypted voice, data, teletype, and facsimile communications, which are interoperable between the United States Army, Navy, Air Force, Marine Corps, and Coast Guard.

Spacecraft

Name Block Launch date/time (UTC) COSPAR ID Rocket Remarks
USA-99 Block I 1994-02-07, 21:47:01 1994-009A Titan IV(401)A
USA-115 Block I 1995-11-06, 05:15:01 1995-060A Titan IV(401)A
USA-143 Block I/II hybrid 1999-04-30, 16:30:00 1999-023A Titan IV(401)B Launch failure
USA-157 Block II 2001-02-27, 21:20 2001-009A Titan IV(401)B
USA-164 Block II 2002-01-16, 00:30:00 2002-001A Titan IV(401)B
USA-169 Block II 2003-04-08, 13:43:00 2003-012A Titan IV(401)B

See also

External links

  • U.S. Air Force fact sheet on MILSTAR
  • MILSTAR 3 / Advanced Extremely High Frequency (AEHF)
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