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Structural dynamics payload loads estimates (Document No: 19830005223)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Engels, R. C. |
| Copyright Year | 1981 |
| Description | The development of a full scale payload integration method which reduces the cost of a load cycle and is capable of land long very large systems is discussed. The method solves the coupled booster/payload system equations and does not involve additional approximations as compared to the standard transient analysis. The method is cost effective and directly applicable to the shuttle payload design case. |
| File Size | 6235100 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830005223 |
| Archival Resource Key | ark:/13960/t1bk6681v |
| Language | English |
| Publisher Date | 1981-08-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Couplings Dynamic Structural Analysis Payload Integration Plan Launch Vehicles Cost Effectiveness Payload Integration Booster Rockets Space Shuttle Payloads Mathematical Models 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 |
