Cryogenic On-Orbit Liquid Depot-Storage, Acquisition and Transfer (COLD-SAT) Experiment Conceptual Design and Feasibility Study

The cryogenic fluid management technologies required for the exploration of the solar system can only be fully developed via space-based experiments. A dedicated spacecraft is the most efficient way to perform these experiments. This report documents the extended conceptual design of the COLD-SAT spacecraft, capable of meeting these experimental requirements. All elements, including the spacecraft, ground segment, launch site modifications and launch vehicle operations, and flight operations are included. Greatly expanded coverage is provided for those areas unique to this cryogenic spacecraft, such as the experiment system, attitude control system, and spacecraft operations. Supporting analyses are included as are testing requirements, facilities surveys, and proposed project timelines.

[1]  Keith Hawkins,et al.  Space vehicle and associated subsystem weight growth , 1988 .

[2]  Hugh Arif.  Spacecraft attitude impacts on COLD-SAT non-vacuum jacketed LH2 supply tank thermal performance , 1990 .

[3]  P. O'Connor,et al.  Practical Reliability Engineering , 1981 .

[4]  J. C. Aydelott.  Modeling of space vehicle propellant mixing. [cryogenic propellants] , 1983 .

[5]  T. N. Stevenson,et al.  Fluid Mechanics , 2021, Nature.

[6]  R. P. Frohmberg,et al.  Hydrogen environment embrittlement of metals , 1973 .

[7]  E. Symons.  Wicking of liquids in screens , 1974 .

[8]  W. Rohsenow,et al.  Handbook of Heat Transfer , 1998 .

[9]  H. N. Abramson,et al.  The Dynamic Behavior of Liquids in Moving Containers, with Applications to Space Vehicle Technology , 1966 .

[10]  Hugh Arif.  Preliminary thermal design of the COLD-SAT spacecraft , 1991 .

[11]  David Linden,et al.  Handbook of batteries and fuel cells , 1984 .

[12]  R. B. Jacobs,et al.  Liquid Requirements for the Cool-Down of Cryogenic Equipment , 1963 .

[13]  E. W. Kroeger,et al.  COLD-SAT: A technology satellite for cryogenic experimentation , 1990 .

[14]  Richard H. Knoll,et al.  Design, Development, and Test of Shuttle/ Centaur G-Prime Cryogenic Tankage Thermal Protection Systems , 1988 .

[15]  I. E. Sumner.  Degradation of a Multilayer Insulation Due to a Seam and a Penetration , 1976 .

[16]  Joseph Moses Juran,et al.  Quality-control handbook , 1951 .

[17]  J. C. Aydelott.  Effect of gravity on self-pressurization of spherical liquid-hydrogen tankage , 1967 .

[18]  Robert D. McCarty,et al.  Hydrogen technology survey: Thermophysical properties , 1975 .

[19]  R. T. Parmley,et al.  Passive Orbital Disconnect Strut , 1984 .

[20]  G. R. Cunnington,et al.  Thermal performance of multilayer insulations. [gas evacuation characteristics of three selected multilayer insulation composites] , 1974 .

[21]  J. C. Aydelott.  Normal gravity self-pressurization of 9-inch- /23 cm/ diameter spherical liquid hydrogen tankage , 1967 .

[22]  Gary Bollenbacher,et al.  COLD-SAT dynamic model , 1992 .

[23]  D. King-hele,et al.  Satellite orbits in an atmosphere : theory and applications , 1987 .

[24]  R. Schlitt,et al.  BATTERY THERMAL DESIGN AND PERFORMANCE IN EUROPEAN GEO-SATELLITE PROGRAMS , 1987 .

[25]  Lawrence G. Edwards,et al.  Cryogenic on-orbit liquid depot storage acquisition and transfer (COLD-SAT) experiment subsystem instrumentation and wire harness design report , 1994 .

[26]  E. P. Symons,et al.  Outlet baffles: Effect on liquid residuals from zero-gravity draining of hemispherically ended cylinders , 1972 .

[27]  J. R. Schuster,et al.  COLD-SAT orbital experiment configured for Atlas launch , 1990 .

[28]  F. R. Schwartzberg,et al.  CRYOGENIC MATERIALS DATA HANDBOOK , 1964 .

[29]  Steven T. Mchenry,et al.  COLD-SAT feasibility study safety analysis , 1991 .

[30]  E. C. Cady,et al.  Study of Thermodynamic Vent and Screen Baffle Integration for Orbital Storage and Transfer of Liquid Hydrogen , 1973 .

[31]  David H. Riemer.  Space station experiment definition: Long term cryogenic fluid storage , 1987 .

[32]  I. E. Sumner.  Liquid propellant reorientation in a low-gravity environment , 1978 .

[33]  P. R. K. Chetty.  Satellite technology and its applications , 1988 .

[34]  William J. Bailey,et al.  Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer satellite (COLD-SAT) feasibility study , 1990 .