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Liquid oxygen propellant densification unit ground tested with a large-scale flight-weight tank for the x-33 reusable launch vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tomsik, Thomas M. |
| Copyright Year | 2002 |
| Description | Propellant densification has been identified as a critical technology in the development of single-stage-to-orbit reusable launch vehicles. Technology to create supercooled high-density liquid oxygen (LO2) and liquid hydrogen (LH2) is a key means to lowering launch vehicle costs. The densification of cryogenic propellants through subcooling allows 8 to 10 percent more propellant mass to be stored in a given unit volume, thereby improving the launch vehicle's overall performance. This allows for higher propellant mass fractions than would be possible with conventional normal boiling point cryogenic propellants, considering the normal boiling point of LO2 and LH2. |
| File Size | 155203 |
| Page Count | 3 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050203875 |
| Archival Resource Key | ark:/13960/t0vq7wj0c |
| Language | English |
| Publisher Date | 2002-03-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Ground Tests Densification Liquid Oxygen X-33 Reusable Launch Vehicle Liquid Hydrogen Reusable Launch Vehicles Cryogenic Rocket Propellants 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 |
