Boeing's Milstar payloads BOEING SATELLITE SYSTEM FACT SHEET Posted: February 25, 2001 Hughes Space and Communications Company (HSC), now known as Boeing Satellite Systems, Inc. (BSS), has been a major part of the Milstar system team since 1982, supplying sophisticated, state-of-the-art radio frequency (RF), microwave, and antenna subsystems hardware. The Milstar system is a tactical and strategic multiservice program involving the Air Force, Army, Navy, and other agencies. Milstar provides protected communications for command and control of the United States war-fighting forces. These include the National Command Authority (NCA), military tactical and strategic forces, Air Force Space Command (AFSPC), and other users. The Program is managed by the U.S. Air Force Space and Missile Systems Center. The Milstar system provides uplink communications at extremely high frequency (EHF), 44 GHz, and ultrahigh frequency (UHF), 300 MHz, and downlink communications at super high frequency (SHF), 20 GHz, and UHF, 250 MHz. It will provide survivable medium data rate (MDR) and low data rate (LDR) communications services between terminals worldwide using crosslinks operating in the 60 GHz region. Survivability and endurability requirements are satisfied by anti-jam, hardening, and system autonomy features. The Milstar system is composed of three segments: the satellite or space segment, the mission control segment, and the terminal segment. The Milstar space segment is procured in two versions. The first two satellites (Milstar 1) provide secure LDR communications. Subsequent satellites (Milstar 2) carry secure MDR communications in addition to the existing secure LDR communications. Milstar 1 and 2 satellites are fully interoperable for LDR communications. Lockheed Martin Space Systems is the prime contractor responsible for the space and mission control segments, as well as system interfaces. Boeing has the prime responsibility for supplying the MDR and crosslink payloads as tactical extensions to the existing robust LDR payload. TRW is the major subcontractor, supplying the MDR antennas and the digital subsystem.
Mission Strategic missions require survivable communications among the NCA, the commanders in chief (CINCs), and other nuclear capable forces. Tactical missions require survivable communications among forces in the same tactical theater and among forces in different tactical theaters. Milstar LDR supports strategic and tactical users' requirements for high anti-jam and nuclear scintillation protection. Milstar MDR will meet the needs of multiple users by supporting the connectivity of tactical and conventional forces.
MDR payload Tactical coverage is provided by the MDR antenna coverage subsystem (ACS), consisting of eight narrow spot beam antennas: two narrow spot beams with nulling capabilities (nuller antennas) and six distributed user coverage antennas (DUCAs), each supporting simultaneous uplink and downlink communications. Narrow spot beams provide good isolation of users from out-of-beam jammers. The nuller antennas resist in-beam jamming by sampling the beamforming elements in the uplink signal, processing correlations, and providing feedback to the beamforming network to null the antenna pattern in the direction of the jammer. The received EHF signal is amplified, de-hopped, and downconverted by the MDR RF subsystem (RFSS). The baseband signal is passed on to the digital subsystem (DSS), for demodulation and routing. The routed signal is passed back to the RFSS for differential phase shift key (DPSK) modulation, hopping upconversion, amplification and filtering. Finally it is switched on a hop-by-hop basis among the eight downlink coverage areas provided by the ACS. The RFSS also supplies the high fidelity frequency references by the MDR payload derived from the references provided by the LDR payload. Uplink/downlink/crosslink connectivity is provided by the DSS. The DSS demodulates uplink baseband data, and deinterleaves and decodes uplink and crosslink messages. It also routes uplink and crosslink data to the appropriate downlink and crosslink, encodes and interleaves downlink and crosslink messages, and provides time tracking responses to terminal uplink timing probes.
Crosslink payload |
Flight data file Vehicle: Titan 4B/Centaur Payload: Milstar 2-F2 Launch date: Feb. 27, 2001 Launch window: 1857-2257 GMT (1:57-5:57 p.m. EST) Launch site: SLC-40, Cape Canaveral AFS, Florida Pre-launch briefing Launch timeline - Chart with the key events to occur during the launch. Titan 4B - Description of America's most powerful unmanned rocket. Milstar satellite - A look at the Military Strategic and Tactical Relay satellite program. Antennas - Technical description of Milstar's medium data rate nulling antennas made by TRW. DPS - TRW's digital processing subsystem on Milstar is key to payload. Restricted zone - Map outlining the Launch Hazard Area where mariners should remain clear for the liftoff. |
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MISSION STATUS CENTER |