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System analysis approach to deriving design criteria (loads) for space shuttle and its payloads. volume 1: general statement of approach
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bullock, T. Kiefling, L. A. Kross, D. A. Ryan, R. S. Holland, W. B. |
| Copyright Year | 1981 |
| Description | Space shuttle, the most complex transportation system designed to date, illustrates the requirement for an analysis approach that considers all major disciplines simultaneously. Its unique cross coupling and high sensitivity to aerodynamic uncertainties and high performance requirements dictated a less conservative approach than those taken in programs. Analyses performed for the space shuttle and certain payloads, Space Telescope and Spacelab, are used a examples. These illustrate the requirements for system analysis approaches and criteria, including dynamic modeling requirements, test requirements control requirements and the resulting design verification approaches. A survey of the problem, potential approaches available as solutions, implications for future systems, and projected technology development areas are addressed. |
| File Size | 2872853 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820006330 |
| Archival Resource Key | ark:/13960/t4nk85t8c |
| Language | English |
| Publisher Date | 1981-12-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Structural Weight Spacelab Engine Design Hubble Space Telescope Launching Pads Structural Design Criteria Systems Analysis Cost Analysis Spacecraft Design Load Distribution Forces Spacecraft Construction Materials Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
