Numerical and experimental comparisons of the self-pressurization behavior of an LH2 tank in normal gravity

Salzman J. Fluid management in space-based systems. In: Engineering, construction, and operations in space, 5th international conference on space, vol. 1; 1996. p. 521–6.

Knoll R, Smolak G, Nunamaker R. Weightlessness experiments with liquid hydrogen in aerobee sounding rockets; uniform radiant heat addition – flight 1. NASA TM X-484; 1962.

Aydelott J, Corpus E, Gruber R. Comparison of pressure rise in a hydrogen dewar for homogeneous, normal-gravity, quiescent, and zero gravity conditions – flight 9. NASA TM X-1052; 1965.

Aydelott J. Normal gravity self-pressurization of 9-inch (23cm) diameter spherical liquid hydrogen tankage. NASA TN D-4171; 1967.

Bailey, 1963, Cryogenic propellant stratification analysis and test data correlation, AIAA J, 1, 1657, 10.2514/3.1875

Arnett R, Voth R. A computer program for the calculation of thermal satisfication and self-pressurization in a liquid hydrogen tank. NASA CR 2026; 1972.

Nguyen H. Zero-g thermodynamic venting system (TVS) performance prediction program. Tech Rep, Rockwell Aerospace; 1994.

Lin C, Hasan M. Self-pressurization of a spherical liquid hydrogen storage tank in a microgravity environment. NASA TM 105372; 1992.

Brown J. Vapor condensation on turbulent liquid. Ph.D. thesis, MIT; 1991.

Hochstein J, Ji H-C, Aydelott J. Effect of subcooling on the on-orbit pressurization rate of cryogenic propellant tankage. AIAA 86–1253; 1986.

Hochstein, 1990, Prediction of self-pressurization rate of cryogenic propellant tankage, J Propul Power, 6, 11, 10.2514/3.23217

Abdalla K, Frysinger T, Androcchio C. Pressure-rise characteristics for a liquid hydrogen dewar for homogeneous, normal gravity, quiescent, and zero-gravity tests. NASA TM X-1134; 1965.

Grayson G, Lopez A, Chandler F, Hastings L, Tucker S. Cryogenic tank modeling for the saturn AS-203 experiment. AIAA 2006-5258; 2006.

Hirt C. Modeling phase change and homogeneous bubbles, FSI-01-TN57. Flow Science Inc.; 2001.

Bradshaw R. Evaluation and application of data from low gravity orbital experiment phase I – final report. NASA CR-109847; 1970.

Navickas, 1968, Propellant behavior during venting in an orbiting saturn S-IVB stage, vol. 13, 188

Merte H, Clark J, Barakat H. Finite difference solution of stratification and pressure rise in containers. Tech rep, Heat Transfer Laboratory, University of Michigan, Tech Report No. 4; 1968.

Merte H et al. Transient pressure rise of a liquid–vapor system in a closed container under variable gravity. In: 4th International heat transfer conference, Paris, France; 1970.

Val’tsiferov, 1975, Convective heat transfer in a closed axisymmetric vessel with curvilinear generatrix in the presence of phase boundaries and phase transitions, Izv Akad Navk SSSR Mekh Ahidk Gaza, 6, 126

Amirkhanyan, 2001, Theoretical analysis and procedure for the calculation of thermophysical processes occurring in a cryogenic vessel under conditions of non-vented storage, High Temp, 39, 905, 10.1023/A:1013103425192

Panzarella, 2003, On the validity of purely thermodynamic descriptions of two-phase cryogenic fluid storage, J Fluid Mech, 484, 41, 10.1017/S0022112003004002

Panzarella, 2005, Self-pressurization of large spherical cryogenic tanks in space, J. Spacecraft Rockets, 42, 299, 10.2514/1.4571

Panzarella, 2004, Pressure control of large cryogenic tanks in microgravity, Cryogenics, 44, 475, 10.1016/j.cryogenics.2004.03.009

Stochl R, Knoll R. Thermal performance of a liquid hydrogen tank multilayer insulation system at warm boundary temperatures of 630, 530, and 152 R. NASA TM 104476; 1991.

Dresar NV, Lin C, Hasan M. Self-pressurization of a flightweight liquid hydrogen tank: effects of fill level at low wall heat flux. NASA TM 105411; 1992.

Hasan M, Lin C, Dresar NV. Self-pressurization of a flightweight liquid hydrogen storage tank subjected to low heat flux. NASA TM 103804; 1991.

Linstrom P, Mallard W, Editors. NIST Chemistry WebBook, NIST Std. Ref. Database Number 69, NIST, 2005, <http://webbook.nist.gov>.

Jacobsen, 1997

Menter F. Zonal two-equation k–w turbulence models for aerodynamic flows. AIAA 93-2906; 1993.