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Rocket propellants engine design/operations/validation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Monk, Jan C. |
| Copyright Year | 2002 |
| Description | Lockheed Martin Astronautics Operations (LMA) was competitively awarded a contract May 21, 2001 for next generation launch system architecture definition and technology maturation. The Second Generation Launch Vehicle Program objectives include reducing the technical and programmatic risk of proceeding to full scale development of the system by establishing requirements for the next generation launch system and maturing critical technologies needed by the system. LMA will conduct analyses and trades to optimize the architecture ETO elements including configuration, conceptual designs, and preliminary operations definition. To fully understand the engine and propellant trades were conducted by LMA to yield the optimized architecture system from the operability, reliability, safety, and cost perspectives. A government/industry team addressed the required trade studies, the parameters and weighting factors, and the most critical trades were addressed. This report summarizes the participation of JCM Consulting, Inc. in the propellant trade study. |
| File Size | 164734 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020029297 |
| Archival Resource Key | ark:/13960/t4cp22g3h |
| Language | English |
| Publisher Date | 2002-02-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Safety Launch Vehicles Rocket Propellants Reliability Engine Design 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 |
