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Rsrm propellant grain geometry modification
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Endicott, Joni B. Schorr, Andrew A. |
| Copyright Year | 2000 |
| Description | This document is composed of viewgraphs about the RSRM propellant grain geometry modification project, which hopes to improve personnel and system safety by modifying propellant grain geometry to improve structural factors of safety. Using techniques such as Finite Element Analysis to determine blend radii required to reduce localized stresses, and ballistic predictions to ensure that the ballistics, ignition transient and Block Model have not been adversely affected, the project hopes to build and test FSM-10 with a new design, and determine flight effectivity pending successful test evaluation. |
| File Size | 481218 |
| File Format | |
| Language | English |
| Publisher Date | 2000-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Finite Element Method Flight Tests Propellant Grains Safety Factors Solid Rocket Propellants Ballistics Safety Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
