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Authors: DESAI PN BRAUN RD POWELL RW ENGELUND WC TARTABINI PV

Citation: Pn. Desai et al., 6-DEGREE-OF-FREEDOM ENTRY DISPERSION ANALYSIS FOR THE METEOR RECOVERYMODULE, Journal of spacecraft and rockets, 34(3), 1997, pp. 334-340

Authors: PHILLIPS WP ENGELUND WC

Citation: Wp. Phillips et Wc. Engelund, AERODYNAMICS FOR A WINGED, CIRCULAR-BODY, SINGLE-STAGE-TO-ORBIT SPACECRAFT CONFIGURATION, Journal of spacecraft and rockets, 34(1), 1997, pp. 43-47

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Authors: STANLEY DO ENGELUND WC LEPSCH R

Citation: Do. Stanley et al., PROPULSION REQUIREMENTS FOR REUSABLE SINGLE-STAGE-TO-ORBIT ROCKET VEHICLES, Journal of spacecraft and rockets, 31(3), 1994, pp. 414-420

Authors: WILHITE AW ENGELUND WC STANLEY DO NAFTEL JC LEPSCH RA BUSH LB WURSTER KE

Citation: Aw. Wilhite et al., TECHNOLOGY AND STAGING EFFECTS ON 2-STAGE-TO-ORBIT SYSTEMS, Journal of spacecraft and rockets, 31(1), 1994, pp. 31-38