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  • ProX DMP 320
  • 기술보고서

    기술보고서 게시판 내용
    타이틀 Concept Design of Cryogenic Propellant Storage and Transfer for Space Exploration
    저자 Free, James M.;; Motil, Susan M.;; Kortes, Trudy F.;; Meyer, Michael L.;; taylor, William J.
    Keyword CRYOGENIC FLUID STORAGE;; CRYOGENIC ROCKET PROPELLANTS;; CRYOGENIC TANKS;; FLIGHT TESTS;; GROUND TESTS;; LIQUID HYDROGEN;; LIQUID OXYGEN;; LONG DURATION SPACE FLIGHT;; METHANE;; MICROGRAVITY;; PROPELLANT STORAGE;; PROPELLANT TRANSFER;; RESEARCH FACILITIES;; SPACE EXPLORATION;; SPACE MISSIONS;; STORABLE PROPELLANTS;; TANK GEOMETRY;; VACUUM CHAMBERS
    URL http://hdl.handle.net/2060/20120016460
    보고서번호 E-18444
    발행년도 2012
    출처 NTRS (NASA Technical Report Server)
    ABSTRACT NASA is in the planning and investigation process of developing innovative paths for human space exploration that strengthen the capability to extend human and robotic presence beyond low Earth orbit and throughout the solar system. NASA is establishing the foundations to enable humans to safely reach multiple potential destinations, including the Moon, asteroids, Lagrange points, and Mars and its environs through technology and capability development. To achieve access to these destinations within a reasonable flight time will require the use of high performance cryogenic propulsion systems. Therefore NASA is examining mission concepts for a Cryogenic Propellant Storage and Transfer (CPST) Flight Demonstration which will test and validate key capabilities and technologies required for future exploration elements such as large cryogenic propulsion stages and propellant depots. The CPST project will perform key ground testing in fiscal year 2012 and *****ute project formulation and implementation leading to a flight demonstration in 2017.

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