Add to ORKGA comprehensive study was performed to develop the major features of a large capacity orbital propellant storage facility for the space-based cryogenic orbital transfer vehicle. Projected propellant usage and delivery schedules can be accommodated by two orbital tank sets of 100,000 lb storage capacity, with advanced missions expected to require increased capacity. Information is given on tank pressurization schemes, propellant transfer configurations, pump specifications, the refrigeration system, and flight tests
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LOX) can dramatically enhance...
The Cryogenic Propellant Storage and Transfer (CPST) project has been a long-running program in the ...
Ground and vehicle system requirements are evaluated for the use of densified cryogenic propellants ...
Long term, cryogenic fluid storage facilities will be required to support future space programs such...
A new era of space exploration is being planned. Exploration architectures under consideration requi...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
(1) Store cryogenic propellants in a manner that maximizes their availability for use regardless of ...
The space community is currently focusing on defining system architectures able to perform multiple ...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
Conceptual designs of Space Transportation Vehicles (STV), and their orbital servicing facilities, t...
NASA Lewis Research Center's Cryogenic Fluid Systems Branch (CFSB) within the Space Propulsion Techn...
As part of U.S. National Space Policy, NASA is seeking an innovative path for human space exploratio...
Mankind is embarking on the next step in the journey of human exploration. We are returning to the m...
Results are summarized for an 11-month study to define fluid storage and handling strategies and req...
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LOX) can dramatically enhance...
The Cryogenic Propellant Storage and Transfer (CPST) project has been a long-running program in the ...
Ground and vehicle system requirements are evaluated for the use of densified cryogenic propellants ...
Long term, cryogenic fluid storage facilities will be required to support future space programs such...
A new era of space exploration is being planned. Exploration architectures under consideration requi...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
(1) Store cryogenic propellants in a manner that maximizes their availability for use regardless of ...
The space community is currently focusing on defining system architectures able to perform multiple ...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
Orbital cryogenic propellant depots and the ability to refuel spacecraft in orbit are critical capab...
Conceptual designs of Space Transportation Vehicles (STV), and their orbital servicing facilities, t...
NASA Lewis Research Center's Cryogenic Fluid Systems Branch (CFSB) within the Space Propulsion Techn...
As part of U.S. National Space Policy, NASA is seeking an innovative path for human space exploratio...
Mankind is embarking on the next step in the journey of human exploration. We are returning to the m...
Results are summarized for an 11-month study to define fluid storage and handling strategies and req...
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LOX) can dramatically enhance...
The Cryogenic Propellant Storage and Transfer (CPST) project has been a long-running program in the ...
Ground and vehicle system requirements are evaluated for the use of densified cryogenic propellants ...