Spacecraft bus definition

Spacecraft bus. (9) means equipment that provides the support infrastructure of the "spacecraft" and location for the "spacecraft payload".
Spacecraft bus. The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function. MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units. Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.e Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.f Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.
Spacecraft bus. The Bus is that part of the Satellite that provides the support infrastructure so the Instrument can function. [**Redacted**]. MGB: “MGB” is a meaningless three letter designation for an additional subsystem being installed on the WV3 satellite. The MGB subsystem consists of three components. The first is a Sensor Unit (SU) which will attach to the aperture end of the OBA. The second is the Interface Adaptor Unit (IAU) which will mount to the spacecraft bus. The third is an inter-connect cable which connects the first two units. Initial Acceptance: Occurs upon successful completion of the Satellite Pre-Ship Review as defined in paragraph 4.5.3.2.d Final Acceptance: Occurs following satellite fueling operations and completion of the Satellite Launch Readiness Review as defined in paragraph 4.5.3.2.e Transfer of Title: Occurs as defined in the Satellite Purchase Agreement paragraph 8.

Examples of Spacecraft bus in a sentence

  • Spacecraft bus testing is often conducted at the observatory level, in which case the Spacecraft PER is performed inconjunction with the Mission PER.

  • It provides the electronic interface between the Spacecraft bus and the Instrument sensors.

  • Spacecraft bus components, as well as some components of the payload electronics, are mounted in enclosures which are then bolted to the body panels.

  • The CTA is mechanically mounted to, but thermally isolated from, the Spacecraft bus by means of low conductivity gamma- alumina struts.

  • The CTA is also thermally isolated from the solar panel and Spacecraft bus by means of low emissivity radiation shields.

  • The solar panel, which is structurally cantilevered from the Spacecraft bus, shades the CTA from the sun at all times.

  • Free Flyers: Provides Spacecraft bus, ground operations and ride-share opportunity.

  • The analysis is based on the JPSS Spacecraft bus design at Spacecraft Critical Design Review (CDR).

  • In addition, approximately 1,300 conductors, forming the cryogenic cable harness, are routed between the MIC and the Spacecraft bus.

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Related to Spacecraft bus

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