Rahul Sharma (Editor)

TacSat 2

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Mission type
  
Technology

COSPAR ID
  
2006-058A

Rocket
  
Minotaur I

Period
  
1.5 hours

Launch mass
  
370 kg

Perigee
  
413,000 m

Operator
  
AFRL

Manufacturer
  
MicroSat Systems

Launch site
  
MARS LP-0B

Launch mass
  
370 kg

Apogee
  
424,000 m

Launch date
  
16 December 2006

TacSat-2 httpsuploadwikimediaorgwikipediacommonsthu

Similar
  
TacSat‑3, TacSat‑4, TacSat‑1, GeneSat‑1, USA‑165

Minotaur i space launch tacsat 2 satellite


TacSat-2 (also known as JWS-D1 or RoadRunner) 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.

Contents

Tacsat 2 launch


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.

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

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.

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

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:

  • RoadRunner Onboard Processing Experiment (ROPE)
  • Common Data Link (CDL)
  • Autonomous Operations
  • Hall Effect Thruster (HET)
  • Propulsion Instrument Electronics (PIE) sensor suite
  • Inertial Stellar Compass (ISC)
  • Low Power Transceiver (LPT)
  • Integrated GPS Occultation Receiver (IGOR)
  • Atmospheric Density Mass Spectrometer (ADMS)
  • Experimental Solar Array
  • Miniaturized Vibration Isolation System (MVIS)
  • Orbit

    The near circular orbit had 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:

  • DOD Space Test Program (Space and Missile Systems Center’s Space Development and Test Wing),
  • Naval Research Laboratory,
  • Army Space Program Office,
  • Air Force Space Command,
  • Space Warfare Center,
  • NASA,
  • Jet Propulsion Laboratory (JPL),
  • Busek
  • References

    TacSat-2 Wikipedia