Loading...
Please wait, while we are loading the content...
Similar Documents
A study of performance and cost improvement potential of the 120 inch (3.05 m) diameter solid rocket motor. volume 1: summary report
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Backlund, S. J. Rossen, J. N. |
| Copyright Year | 1971 |
| Description | A parametric study of ballistic modifications to the 120 inch diameter solid propellant rocket engine which forms part of the Air Force Titan 3 system is presented. 576 separate designs were defined and 24 were selected for detailed analysis. Detailed design descriptions, ballistic performance, and mass property data were prepared for each design. It was determined that a relatively simple change in design parameters could provide a wide range of solid propellant rocket engine ballistic characteristics for future launch vehicle applications. |
| File Size | 1087085 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720007149 |
| Archival Resource Key | ark:/13960/t3kx0575t |
| Language | English |
| Publisher Date | 1971-12-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Solid Propellant Rocket Engines Performance Prediction Rocket Engine Control Cost Analysis Engine Design Systems Engineering 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 |
