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GP-B Post-Flight Analysis—Final Report - Gravity Probe B - Stanford ...

GP-B Post-Flight Analysis—Final Report - Gravity Probe B - Stanford ...

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Among the reasons for NASA’s decision to make <strong>Stanford</strong> the prime contractor on <strong>GP</strong>-B were the following:1. The payload and spacecraft were intimately interdependent. That is, the payload sensor was the keycontrol element to the space vehicle system. One of the four science gyros was also used as the drag-freesensor, and the helium gas escaping from the dewar was used by proportional micro-thrusters tomaintain drag-free and attitude control. The total-system mass center location was also critical.2. The development process and specification derivation were integrated. Because the payload drove mostof the spacecraft requirements, the specifications were linked. They were developed together and verifiedin an integrated fashion.3. Many of the technologies associated with the science Instrument Assembly—namely, the gyroscopes andtheir suspension systems, the SQUIDs, and the pointing telescope—were entirely new and uniquetechnologies that could only have been developed in a very advanced academic research environment.4. The Science Instrument Assembly had to be integrated into the probe, the probe was then integrated intothe dewar, and finally, the dewar-probe unit was integrated into the spacecraft, so that all of thesecomponents functioned together as a unified system. This total integration of payload and spacecraft wascrucial to the success of the mission.5. The scientists and engineers at <strong>Stanford</strong> understood points 1-4 above, and they were the logical peopleable to oversee the technical trade-offs associated with designing and constructing this unique spacecraft.In November 1984, following a by-the-book competitive bidding process, <strong>Stanford</strong> selected Lockheed Martin tobuild the flight dewar and probe that would house the Science Instrument Assembly, the heart of theexperiment being developed and constructed at <strong>Stanford</strong>. <strong>GP</strong>-B then sent MSFC/NASA Headquarters aproposal, with <strong>Stanford</strong> as the prime contractor and LM as <strong>Stanford</strong>'s subcontractor, for implementing therestructured flight plan and building the required flight hardware. In 1985, MSFC/NASA Headquartersaccepted the <strong>Stanford</strong>-Lockheed Martin STORE proposal and funded this technology development plan. Thefact that the technology plan included LM as <strong>Stanford</strong>'s industry subcontractor represented a significantincrease in management responsibility for <strong>Stanford</strong>. However, under Parkinson's experience and leadership,<strong>Stanford</strong> was prepared for this challenge, and “The Management Experiment” commenced.6.3 <strong>Flight</strong> Hardware Development (1984-1997)James Beggs, the NASA Administrator in 1985, concurred with Samuel Keller's decision to make <strong>Stanford</strong> thePrime Contractor on <strong>GP</strong>-B, and he remarked that in addition to being a physics experiment that needed to becarried out in space, <strong>GP</strong>-B was equally interesting as a “management experiment.”As stated in the Calder-Jones <strong>Report</strong> to NASA, page 7:The Management Experiment was an agreement between NASA Headquarters, NASAMSFC, and <strong>Stanford</strong> University that established <strong>Stanford</strong> as the prime contractor, managingthe entire program with minimal NASA oversight. The decision followed a recommendationfrom the Space Studies Board (SSB) to NASA Headquarters in mid-1983, after the SSB hadreviewed the MSFC Phase B Study. The view of the SSB, endorsed by NASA Headquarters,was that in a mission such as <strong>GP</strong>-B where the instrument and spacecraft are much moreclosely integrated than in typical space programs, separating the two would be gravelydetrimental. It was predicated on <strong>Stanford</strong> University's agreeing to set up a much strongermanagement structure than is typical in universities.The flight hardware development period continued for about 15 years, at which time it became necessary totransition <strong>GP</strong>-B from a research and development program with minimal NASA oversight to a classical NASAflight program that would culminate in a successful launch, on-orbit operations, and subsequent data analysis,leading to the determination of the experimental results.<strong>Gravity</strong> <strong>Probe</strong> B — <strong>Post</strong> <strong>Flight</strong> Analysis • Final <strong>Report</strong> March 2007 149

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