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Spacecraft Requirements Development and TailoringSpacecraft design is managed through the use of design requirements. Requirements are flowed from the highest level, the overall spacecraft, to systems, subsystems and ultimately individual components. Through the use of requirements, each part of the spacecraft will perform the functions that are required of it and will interface to the rest of the spacecraft. Functional requirements are used to make sure every component performs as expected and interface requirements ensure that each component works within the larger design environment where it operates. Writing good requirements is difficult and the verification of requirements can be expensive and time consuming. Because of this difficulty and expense, it is important that each requirement truly be “required” and critical to the overall performance of the vehicle. It is also important that requirements can be changed or eliminated as the system matures to minimize verification cost and schedule. The Capsule Parachute Assembly System (CPAS) Project is developing the parachute system for the NASA Multi-Purpose Crew Vehicle (MPCV) Orion Spacecraft. Throughout the development and qualification cycle for CPAS, requirements have been evaluated, added, eliminated, or more generically, “tailored”, to ensure that the system performs as required while minimizing the verification cost to the Program. One facet of this tailoring has been to delete requirements that do not add value to the overall spacecraft or are not needed. A second approach to minimize the cost of requirement verification has been to evaluate requirements based on the actual design as it has matured. As the design of the parachute system has become better understood, requirements that are not applicable have been eliminated. This paper will outline the evolution of CPAS requirements over time and will show how careful and considered changes to requirements can benefit the technical solution for the overall system design while allowing a Project to control costs.
Document ID
20200001578
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Mcmichael, James H.
(NASA Johnson Space Center Houston, TX, United States)
Mccann, Charles J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
March 13, 2020
Publication Date
June 17, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-E-DAA-TN68246
Report Number: JSC-E-DAA-TN68246
Meeting Information
Meeting: AIAA Aviation Forum and Expo
Location: Dallas, TX
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2020
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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