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OSC: MicroStar

MicroStar (Orbcomm) [OSC]

MicroStar (double)
(OrbView 1) [OSC]

BATSAT (Teledesic T1) [OSC]

MicroStar-2 (generic) [Orbital]

Designed to be launched in multiple or "piggyback" units, Orbital'sinnovativeMircroStar satellite platform supports payloads up to 68 kgand provides a three- to five-year mission life. The baseline bus is comprised of threerings stacked together vertically – a core ring housing all primary spacecraft bussystems and a payload support module consisting of two rings and a payload mounting shelf.Payloads requiring different depths can be easily accommodated by using fewer rings, or bycreating a custom ring. The open avionics architecture, stackable mechanical design andscalable spacecraft design maximize payload performance and flexibility.

The MicroStar configuration is applicable for a variety of missions, from technologydemonstrations to space science programs such asQuikTOMS.MicroStar is also an ideal bus for science missions that require simultaneous deploymentof multiple spacecraft, as in certain magnetospheric and ionospheric investigations.

Using a production line approach for assembly and testing, Orbital has delivered 38MicroStar spacecraft, including 26Orbcommsatellites launched in 10 months. This approach provides cost and schedule advantagesthrough the use of mature designs, familiar manufacturing and test equipment, dedicatedand experienced personnel, and established vendor sources. The production line hasremained in place to supportOrbcomm spares andindividual MicroStar missions such asT1 andMUBLCOM. NASA'sQuikTOMSspacecraft is also taking advantage of this production line.

MicroStar's unique, stackable design offers frequent, cost-effectivelaunch-sharing opportunities. For example, eightOrbcommsatellites are launched at one time on a Pegasus. While MicroStar is optimized forOrbital'sPegasus andTaurus launch vehicles, it can fly on other vehicles aswell.

Customers can purchase the MicroStar spacecraft alone, or as part of a turn-key servicethat includes operations and data delivery as well. For theOrbView 1 program, Orbital provided end-to-endpayload services. The company produced the satellite bus, integrated two payloads, andlaunched the satellite on Pegasus.

The MicroStar platform was originally developed to support theOrbcomm wireless data communications system, whichprovides real-time, mobile, two-way data and messaging communications services worldwide.The first three MicroStar units,Orbcomm FM-1 & -2and theOrbView 1 remote sensing satellite, werelaunched on a single Pegasus in April 1995. Entering their fifth year of operation, thesesatellites continue to operate reliably.

The MicroStar-2 platform replaces the ring structure by a hexagonal structure.

SatelliteDateLauncherWeight (kg)Remarks
LaunchBOL
Microstar (Single)
FORMOSAT 3A (COSMIC 1)(ex ROCSAT 3A)15.04.2006Minotaur-170
FORMOSAT 3B (COSMIC 2)(ex ROCSAT 3B)15.04.2006Minotaur-170
FORMOSAT 3C (COSMIC 3)(ex ROCSAT 3C)15.04.2006Minotaur-170
FORMOSAT 3D (COSMIC 4)(ex ROCSAT 3D)15.04.2006Minotaur-170
FORMOSAT 3E (COSMIC 5)(ex ROCSAT 3E)15.04.2006Minotaur-170
FORMOSAT 3F (COSMIC 6)(ex ROCSAT 3F)15.04.2006Minotaur-170
MUBLCOM18.05.1999Pegasus-XL HAPS48
Orbcomm FM01 (F1)03.04.1995Pegasus-H40
Orbcomm FM02 (F2)03.04.1995Pegasus-H40
Orbcomm FM03 (G1)10.02.1998Taurus-221040
Orbcomm FM04 (G2)10.02.1998Taurus-221040
Orbcomm FM05 (A1)23.12.1997Pegasus-XL HAPS40
Orbcomm FM06 (A2)23.12.1997Pegasus-XL HAPS40
Orbcomm FM07 (A3)23.12.1997Pegasus-XL HAPS40
Orbcomm FM08 (A4)23.12.1997Pegasus-XL HAPS40
Orbcomm FM09 (A5)23.12.1997Pegasus-XL HAPS40
Orbcomm FM10 (A6)23.12.1997Pegasus-XL HAPS40
Orbcomm FM11 (A7)23.12.1997Pegasus-XL HAPS40
Orbcomm FM12 (A8)23.12.1997Pegasus-XL HAPS40
Orbcomm FM13 (B1)02.08.1998Pegasus-XL HAPS40
Orbcomm FM14 (B2)02.08.1998Pegasus-XL HAPS40
Orbcomm FM15 (B2)02.08.1998Pegasus-XL HAPS40
Orbcomm FM16 (B4)02.08.1998Pegasus-XL HAPS40
Orbcomm FM17 (B5)02.08.1998Pegasus-XL HAPS40
Orbcomm FM18 (B6)02.08.1998Pegasus-XL HAPS40
Orbcomm FM19 (B7)02.08.1998Pegasus-XL HAPS40
Orbcomm FM20 (B8)02.08.1998Pegasus-XL HAPS40
Orbcomm FM21 (C1)23.09.1998Pegasus-XL HAPS40
Orbcomm FM22 (C2)23.09.1998Pegasus-XL HAPS40
Orbcomm FM23 (C3)23.09.1998Pegasus-XL HAPS40
Orbcomm FM24 (C4)23.09.1998Pegasus-XL HAPS40
Orbcomm FM25 (C5)23.09.1998Pegasus-XL HAPS40
Orbcomm FM26 (C6)23.09.1998Pegasus-XL HAPS40
Orbcomm FM27 (C7)23.09.1998Pegasus-XL HAPS40
Orbcomm FM28 (C8)23.09.1998Pegasus-XL HAPS40
Orbcomm FM29 (D1)cancelledPegasus-XL HAPS45rebuilt asTACSAT 1
Orbcomm FM30 (D2)04.12.1999Pegasus-XL HAPS45
Orbcomm FM31 (D3)04.12.1999Pegasus-XL HAPS45
Orbcomm FM32 (D4)04.12.1999Pegasus-XL HAPS45
Orbcomm FM33 (D5)04.12.1999Pegasus-XL HAPS45
Orbcomm FM34 (D6)04.12.1999Pegasus-XL HAPS45
Orbcomm FM35 (D7)04.12.1999Pegasus-XL HAPS45
Orbcomm FM36 (D8)04.12.1999Pegasus-XL HAPS45
Orbcomm FM37 (E1)cancelledPegasus-XL HAPS45
Orbcomm FM38 (E2)cancelledPegasus-XL HAPS45
Orbcomm FM39 (E3)cancelledPegasus-XL HAPS45
Orbcomm FM40 (E4)cancelledPegasus-XL HAPS45
Orbcomm FM41 (E5)cancelledPegasus-XL HAPS45
Orbcomm FM42 (E6)cancelledPegasus-XL HAPS45
Orbcomm FM43 (E7)cancelledPegasus-XL HAPS45
Microstar (Double)
OrbView 1 (Microlab 1)03.04.1995Pegasus-H68
QuikTOMS21.09.2001FTaurus-2110166Launch Failure
SBD21.09.2001FTaurus-211073Launch Failure
Microstar (Triple)
BATSAT (Teledesic T1)26.02.1998Pegasus-XL120
TacSat 1(exOrbcomm F29)?Falcon-1110
MicroStar-2
IBEX (SMEX 10, Explorer 91)19.10.2008Pegasus-XL [Star-27H]105
ST 82009Pegasus-XL246cancelled
Further DSI / CTA / OSC satellite busses:

Source: OSC Microstar Data Sheet

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Last update: 14.01.2023
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