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Expendable second stage reusable space shuttle booster. volume 4: detail mass properties data
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1971 |
| Description | Mass properties data are presented to describe the characteristics of an expendable second stage with a reusable space shuttle booster. The final mass characteristics of the vehicle configurations for three specified payloads are presented in terms of weight, center of gravity, and mass moments of inertia. Three basic subjects are the integrated vehicle system, the expendable second stage, and the booster modifications. |
| File Size | 2159401 |
| Page Count | 93 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730006143 |
| Archival Resource Key | ark:/13960/t3xt0g73n |
| Language | English |
| Publisher Date | 1971-06-25 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Mass Balance Spacecraft Performance Mass Distribution Spacecraft Stability Reusable Spacecraft Aerodynamic Characteristics Spacecraft Configurations Space Shuttle Boosters Payloads 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 |
