Loading...
Please wait, while we are loading the content...
Similar Documents
Water pressure and accelerations during landing of a dynamic model of the apollo spacecraft with a deployed-heat-shield impact-attenuation system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system |
| File Size | 2934729 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680009353 |
| Archival Resource Key | ark:/13960/t2z36k00c |
| Language | English |
| Publisher Date | 1968-03-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |