1. 4Sutton, G.P. Rocket Propulsion Elements, SixthEdition,JohnWiley&Sons,Inc.,NY,USA,1992. Sutherland,G.and Maes, M. " A Review of Microrocket Technology: 10"6to 1 IbfThrust," Journal of Spacecraft and Rockets, Vol.3, 1966, pp.1153-1163. ^othe, D. E. "Electron-Beam Studies of Viscous Flow in Supersonic Nozzles,"AIAA Journal, Vol. 9, No.5, 1971,pp.804-811.7Rae, W. J. "Some Numerical Results on Viscous Low-Density Nozzle Flows in the Slender Channel Approximation,"AIAA Journal, Vol. 9, No. 5, 1971, pp.811-820. Driscoll, R. J. "Study of the Boundary Layers in Chemical Laser Nozzles," AIAA Journal, Vol. 14, No. 11, 1974,pp. 870-872.9Whitfild, D.L.,andLewis, C.H."Boundary-Layer Analysis of Low Density Nozzle including Displacement, Slip, and Transverse Curvature," Journal of Spacecraft and Rocket, Vol. 7, No. 4, 1970,pp.462-468.10Greenberg, R. A. "Rapid Expansion Nozzles for Gas Dynamic Lasers," AIAA Journal, Vol. 10, no. 11, 1972,pp. 1494-1498.11Whitfield, D. L. "Theoretical and Experimental Investigation of Boundary Lasyers in Low Density Hypersonic Axisymmetric Nozzles," AEDC-TR-68-193,1968.12Murch, C. K. "LowThrust Nozzle Performance," AIAAPaper 68-91,1968.13Bayt, R. L., Ayon, A.A. & Breuer, K. S. "A Performance Evaluation of MEMS-based Micronozzles,"AIAAPaper 97-3169., 1997. "Janson, S. W., Helvajian, H., Hansen, W. "Batch-Fabricated CW Microthrusters: for Kilogram Class Spacecraft," 1999,AIAApaper 99-2722.