Distribution of neutral propellant from electric thrusters onto spacecraft components
作者： E. A. Richley , T. W. Reynolds
DOI:
关键词: Condensation 、 Physics 、 Propellant 、 Electrically powered spacecraft propulsion 、 Spacecraft 、 Distribution (number theory) 、 Aerospace engineering
摘要:
参考文章(7)
T. W. Reynolds, E. A. Richley, Free-molecule flow and surface diffusion through slots and tubes A summary ,(1967)
R. R. Hibbard, C. H. Liebert, Theoretical temperatures of thin-film solar cells in earth orbit ,(1968)
E.W. Spisz, J.R. Jack, Thermal radiative and electrical properties of a cadmium sulfide solar cell at low solar intensities and temperatures Lewis Research Center,Cleveland. ,(1968)
DAVID F. HALL, BRIAN E. NEWNAM, JAMES R. WOMACK, Electrostatic rocket exhaust effects on solar- electric spacecraft subsystems Journal of Spacecraft and Rockets. ,vol. 7, pp. 305- 312 ,(1969) , 10.2514/3.29925
JOHN F. STAGGS, WILLIAM P. GULA, WILLIAM R. KERSLAKE, Distribution of neutral atoms and charge- exchange ions downstream of an ion thruster. Journal of Spacecraft and Rockets. ,vol. 5, pp. 159- 164 ,(1968) , 10.2514/3.29208
H. G. Nöller, Approximate Calculation of Expansion of Gas from Nozzles into High Vacuum Journal of Vacuum Science and Technology. ,vol. 3, pp. 202- 207 ,(1966) , 10.1116/1.1492475
W. J. Parker, G. L. Abbott, Theoretical and Experimental Studies of the Total Emittance of Metals Thermal Radiation of Solids. ,vol. 55, pp. 11- ,(1965)