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NASA Sounding Rocket Program Handbook. - NASA Visitor Center ...

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810-HB-SRP<br />

all with responsibility aware of the current design plans. The design of the payload should be<br />

completed in order for a DR to be held. If this is not possible because of schedule<br />

constraints, the review should be held as soon as a design has been completed that is<br />

sufficient to allow a thorough review. <strong>NASA</strong>, NSROC, and customer representatives may<br />

attend the DR and assign action items as necessary<br />

• Pre-DR Process: Should a DR be required, the following process is used to request,<br />

initiate, conduct, document and respond to action items issuing from it:<br />

1) The MM, in conjunction with the PI, schedules the Design Review and<br />

coordinates the Project Team’s preparedness.<br />

2) The NSROC Contractor establishes a Design Review Panel that reviews all<br />

aspects of the mission, vehicle, design, test plan and integration activities.<br />

The Panel consists of NSROC personnel who are not directly involved with<br />

the mission but who have established expertise in the areas of technical<br />

support required for mission success. These include: Flight Performance,<br />

Mechanical Systems, Electrical Systems, Instrumentation Systems, Guidance,<br />

Navigation and Control Systems, Recovery Systems, Launch Vehicle<br />

Systems, and Ground and Flight Safety (<strong>NASA</strong> personnel).<br />

3) The NSROC Mission Manager formally announces the DR, specifying the<br />

subject flight mission, date, time, and place.<br />

• The Design Review Meeting: During the DR, the Mission Team formally and<br />

systematically presents all information necessary to demonstrate that the proposed<br />

design and mission approach can meet all mission and safety requirements. The<br />

customer should be prepared to discuss all details of the scientific instrument design<br />

and interface with the support systems.<br />

The PI Data Package for a Design Review can be found in Appendix D and includes:<br />

• Complete mission and vehicle design information including all subsystems on<br />

the payload and vehicle.<br />

• Complete descriptions of the proposed test plan for the complete payload and<br />

each system associated with the mission<br />

• A listing of all procedures involving hazardous operations, safety-related<br />

issues, and assembly of the launch vehicle and payload.<br />

17

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