Loading...
Please wait, while we are loading the content...
System analysis approach to deriving design criteria (loads) for space shuttle and its payloads. volume 2: typical examples
| 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 | The achievement of an optimized design from the system standpoint under the low cost, high risk constraints of the present day environment was analyzed. Space Shuttle illustrates the requirement for an analysis approach that considers all major disciplines (coupling between structures control, propulsion, thermal, aeroelastic, and performance), simultaneously. The Space Shuttle and certain payloads, Space Telescope and Spacelab, are examined. The requirements for system analysis approaches and criteria, including dynamic modeling requirements, test requirements, control requirements, and the resulting design verification approaches are illustrated. A survey of the problem, potential approaches available as solutions, implications for future systems, and projected technology development areas are addressed. |
| File Size | 9667399 |
| Page Count | 128 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820007233 |
| Archival Resource Key | ark:/13960/t1xd5qf8v |
| Language | English |
| Publisher Date | 1981-12-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Spacelab Aerospace Vehicles Systems Engineering Space Shuttles Hubble Space Telescope Structural Design Criteria Dynamic Loads Design Analysis Spacecraft Design Aerospace Systems Payloads Loads Forces 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 |
