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Cost modeling techniques for design maturity. [of reentry vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ruhland, E. W. |
| Copyright Year | 1974 |
| Description | Cost modeling techniques and factors which either add to or subtract from these estimates are examined. The most important factors for increasing costs are interfacing subsystems, subsystem design and software maturity. Cost decrease depends on hardware, software, and support equipment availability. A cost modeling analysis for reentry shield and aerodynamic decelerator subsystems of a reentry vehicle is presented. Integration problems for the subsystems are also discussed. |
| File Size | 534530 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750012341 |
| Archival Resource Key | ark:/13960/t42r8m81n |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Cost Estimates Spacecraft Components Deceleration Space Probes Heat Shielding Reentry Vehicles Design Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
