Title :
Implementation approach for Discovery-class missions
Author :
Vellinga, Joseph M.
Author_Institution :
Lockheed Martin Astronaut. Oper., Denver, CO, USA
Abstract :
A sound implementation approach is necessary to win Discovery missions and is critical to successfully accomplishing the mission. The science concept is iterated with the design and implementation approach until a mission is defined that is within the 35-month development to launch period and the cost cap, and utilizes technology that permits implementation with acceptable program risk. The original mission concept must be defined in sufficient depth that development risks are low and the costs are well defined. This takes a very cooperative total team effort and willingness to be flexible to develop a balanced total mission package. Once selected the team must then commit to implement the mission within the agreement. This paper addresses the end-to-end implementation using Stardust, the fourth Discovery mission as a model. The author managed the industrial partner effort for Stardust development
Keywords :
aerospace computing; aerospace control; costing; planetary rovers; risk management; space research; space vehicles; Discovery-class missions; Stardust; acceptable program risk; balanced total mission package; comet samples; cooperative total team effort; cost cap; development risks; development to launch period; end-to-end implementation; implementation approach; return capsule; science requirements; software development; Costs; Earth; IEEE news; Laboratories; Mars; NASA; Packaging; Proposals; Space vehicles; Testing;
Conference_Titel :
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-6599-2
DOI :
10.1109/AERO.2001.931692