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Microstar
Formosat 3A FM6
Formosat 3A FM6
Credit: Manufacturer Image
American communications technology satellite. Small satellite bus, specially designed for multiple launch by Pegasus or Taurus family launch vehicles.

AKA: Formosat;IBEX;Microlab;MUBLCOM;QuikTOMS. Status: Operational 1995. First Launch: 1995-04-03. Last Launch: 2008-10-19. Number: 22 . Gross mass: 43 kg (94 lb).

Notably used for the Orbcomm LEO network for global communications and related spacecraft.

Orbital's MicroStar was a commercially-produced spacecraft bus designed for multiple launch by Orbital's Pegasus or Taurus launch vehicles. MicroStar supported payloads up to 68 kg and provides a three to five-year mission life. The baseline bus was comprised of three rings stacked together vertically -- a core ring housing all primary spacecraft bus systems and a payload support module consisting of two rings and a payload mounting shelf. Payloads requiring different depths could be accommodated by using fewer rings, or by creating a custom ring. The open avionics architecture, stackable mechanical design and scalable spacecraft design maximize payload performance and flexibility.

Using a production line approach for assembly and testing, Orbital delivered over 38 MicroStar spacecraft, including 26 ORBCOMM satellites launched in 10 months in 1995-1996. This approach provided cost and schedule advantages through the use of mature designs, familiar manufacturing and test equipment, dedicated and experienced personnel, and established vendor sources. The production line remained in place to support ORBCOMM spares and individual MicroStar missions such as T1 and MUBLCOM. NASA's QuikTOMS spacecraft also took advantage of this production line.

Customers could purchase the MicroStar spacecraft alone, or as part of a turn-key service that includes operations and data delivery as well. For the OrbView-1 and OrbView-2 programs, Orbital provided end-to-end payload services. The company produced the satellite bus, integrated two payloads, and launched the satellite on Pegasus. Orbital conducted mission operations from its own ground station delivering data to principal investigators via direct downlink and the Internet. H

The MicroStar platform was originally developed to support the ORBCOMM wireless data communications system, which provided real-time, mobile, two-way data and messaging communications services worldwide. The first three MicroStar units, ORBCOMM FM-1&-2 and the OrbView-1 remote sensing satellite, were launched on a single Pegasus in April 1995.

Core Technical Specifications

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Subtopics

Orbcomm Orbital Communications Corp, Dulles, USA. Orbcomm was a commercial venture to provide global messaging services using a constellation of 26 low-Earth orbiting satellites. Communication (Data) satellite built by Orbital Sciences Corporation (OSC) for Orbcomm, USA. Launched 1995 - 1999. Used the MicroStar bus.

OrbView 1 (MicroLab 1) Null

BATSAT (Teledesic T1) Null

MUBLCOM The disk-shaped MUBLCOM satellite used the [Microstar] bus.

QuikTOMS The QuikTOMS satellite was a NASA-GSFC project carrying the TOMS-5 ozone mapper. QuikTOMS used a 168 kg double [Microstar] bus and was to have replaced TOMS instruments on a delayed Russian weather satellite and the failed ADEOS.

SBD American technology satellite. SBD, the Orbital Corporation Special Bus Design, was a 73 kg test version of an enlarged Microstar bus. Technology satellite for Orbital Sciences Corporation (OSC), USA. Launched 2001. Used the MicroStar (double) bus.

FORMOSAT 3 / COSMIC (S00-8) Null

IBEX (SMEX 10) Null

ST 8 Technology satellite built by Orbital Sciences Corporation (OSC) for NASA. Used the MicroStar-2 bus.

TacSat 1A Technology, imaging satellite built by Naval Force Research Laboratory (NRL); Orbital Science Corporation (OSC): bus for Naval Force Research Laboratory (NRL). Used the MicroStar (triple) bus.

Family: Astronomy, Communications, Communications technology sat, Earth, Technology. Country: USA. Spacecraft: Orbcomm. Launch Vehicles: Minuteman, Pegasus, Taurus, Pegasus XL, Pegasus H, Pegasus XL/HAPS, Taurus 2210, Taurus 2110, Minotaur, Minotaur 1. Launch Sites: Vandenberg, Vandenberg 576E, Point Arguello WADZ, Wallops Island DZ, Vandenberg SLC8, Kwajalein DZ. Bibliography: 2, 276, 4, 552, 554, 6, 6707, 12832, 12833.
Photo Gallery

Teledesic 1Teledesic 1
Credit: Manufacturer Image


IBEXIBEX
Credit: Manufacturer Image


MUBLCOMMUBLCOM
Credit: Manufacturer Image


Orbcomm B5Orbcomm B5
Credit: Manufacturer Image


Orbview-1Orbview-1
Credit: Manufacturer Image


QuikTOMSQuikTOMS
Credit: Manufacturer Image


ST 8ST 8
Credit: Manufacturer Image


Tacsat 1Tacsat 1
Credit: Manufacturer Image



1991 July 17 - . 01:46 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 40.
1993 April 25 - . 13:56 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Edwards.. Launch Platform: NB-52 008. Launch Vehicle: Pegasus.
1995 April 3 - . 13:48 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.
1997 December 23 - . 19:11 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island DZ. Launch Pad: RW04/22. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS.
1998 February 10 - . 13:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Taurus. Launch Vehicle: Taurus 2210.
1998 August 2 - . 16:24 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island DZ. Launch Pad: RW04/22. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS.
1998 September 23 - . 05:06 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island DZ. Launch Pad: RW04/22. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS.
1999 May 18 - . 05:09 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS.
1999 December 4 - . 18:53 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island DZ. Launch Pad: RW04/22. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS.
2001 September 21 - . 18:49 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Taurus. Launch Vehicle: Taurus 2110. FAILURE: A problem a few seconds after first stage separation caused the rocket to go off course; it recovered and the remainder of the stages fired, but final cutoff velocity was too low to reach a sustainable orbit..
2006 April 15 - . 01:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC8. LV Family: Minuteman. Launch Vehicle: Minotaur 1.
2008 June 19 - . 06:36 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
2008 October 19 - . 17:47 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein DZ. Launch Pad: RW06/24. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL.

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