Title :
Integration and test for small shuttle payloads
Author :
Wright, Michael R.
Author_Institution :
Dept. Flight Syst. Integration & Test, NASA Goddard Space Flight Center, Greenbelt, MD, USA
Abstract :
Recommended approaches for small space shuttle payload integration and test (I&T) are presented. The paper is intended for consideration by developers of small shuttle payloads, including I&T managers, project managers, and system engineers. Examples and lessons learned are presented based on the extensive history of NASA\´s Hitchhiker project. All aspects of I&T are presented, including: I&T team responsibilities, coordination, and communication; flight hardware handling practices; documentation and configuration management; I&T considerations for payload development; I&T at the development facility; prelaunch operations, transfer, orbiter integration and interface testing; and postflight operations. This paper is of special interest to those payload projects that have small budgets and few resources: that is, the truly "faster, cheaper, better" projects. All shuttle small payload developers are strongly encouraged to apply these guidelines during I&T planning and ground operations to take full advantage of today\´s limited resources and to help ensure mission success.
Keywords :
aerospace testing; configuration management; space vehicles; system documentation; Hitchhiker project; communication; configuration management; coordination; development facility; documentation; flight hardware handling practices; ground operations; interface testing; orbiter integration; payload development; payload integration and test; small shuttle payloads; team responsibilities; Aerospace engineering; Document handling; Engineering management; Hardware; History; Payloads; Project management; Space shuttles; Systems engineering and theory; Testing;
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
DOI :
10.1109/AERO.2002.1036834