TacSat-2

TacSat-2

Artist's rendering of TacSat-2
Mission type Technology
Operator AFRL
COSPAR ID 2006-058A
Spacecraft properties
Manufacturer MicroSat Systems
Launch mass 370 kilograms (820 lb)
Start of mission
Launch date December 16, 2006 (2006-12-16)
Rocket Minotaur I
Launch site MARS LP-0B
Contractor Orbital
End of mission
Decay date February 5, 2011
Orbital parameters
Reference system Geocentric
Regime Low Earth
Eccentricity 0.00080924004
Perigee 413 kilometers (257 mi)
Apogee 424 kilometers (263 mi)
Inclination 40& degrees
Period 92.9 minutes

TacSat-2 (also known as JWS-D1 or RoadRunner)[1] is an experimental satellite built by the USAF's Air Force Research Laboratory with an operational life expected to be not more than one year as part of the 'Advanced Concept Technology Demonstration' program.

Purpose

The TacSat series of experimental spacecraft are designed to allow military commanders on a battlefield to request and obtain imagery and other data from a satellite as it passes overhead. Collected data will be delivered to field commanders in minutes rather than hours or days. The sensor on TacSat-2 can collect color images sharp enough to distinguish ground objects as small as 1 meter in diameter.[2]

Launch

TacSat-2 was launched on 16 December 2006 from the Mid-Atlantic Regional Spaceport using an Orbital Sciences Minotaur launch vehicle. The Mid-Atlantic Regional Spaceport is a commercial space launch facility located on the Delmarva Peninsula 5 miles (8.0 km) west of Chincoteague, Virginia.

Systems

Satellites in the TacSat series were planned to use commercial or available launchers, and largely off-the-shelf components, in order to reduce costs.

Platform

The space platform was built by MicroSat Systems of Littleton, Colorado. The core avionics of the spacecraft including command and data handling, electrical power switching and distribution, and subsystem & payload interfaces is handled by an Integrated Avionics Unit (IAU) developed by Broad Reach Engineering. The spacecraft flight software consists of the low level drivers, and bus manager functionality provided by Broad Reach Engineering, ADCS Software by ASI, and a number of higher level applications by 3rd parties, most notably the Autonomous Tasking Experiment (ATE) by Interface & Control Systems.

Camera / Telescope

TacSat-2 during integration

The developers originally asked for bids from contractors for a camera. These were priced at around US$10 million. The team then bought a high-end observatory telescope costing around $20,000 and added a camera sensor ($2 million), delivering a sensor capable of 1m ground resolution.[3]

The telescope has 50 cm (0.5 m) aperture and was from RC Optical Systems.[4]

Signals Intelligence

A signals intelligence payload, called the Target Indicator Experiment, detects radio wave emitters and can be used in concert with receivers on other platforms such as the US Navy's P-3C maritime patrol aircraft.

Other systems include:

Orbit

The orbit is planned to have a height of 410 km at an inclination of 40 degrees to the equator. TacSat-2 decayed on February 5, 2011.

Developers

Apart from the Air Force Research Laboratory (AFRL), other organisations participating included:

See also

References

  1. ↑ http://pdf.aiaa.org/preview/CDReadyMSPACE05_1181/PV2005_6830.pdf Accessed 28 June 2007
  2. ↑ Singer, Jeremy (2006-12-04). "USAF To Experiment With Satellite To Improve Ground Communications". Defense News.
  3. ↑ Singer, Jeremy (2006-12-07). "TacSat-2 Ushers in New Era in Satellite Operations". Space News. Retrieved 2008-08-07.
  4. ↑ Astronautix - Tacsat2
  5. ↑ "Integrated GPS Occultation Receiver". Broad Reach Engineering.
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