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Results: 1-7 |
Results: 7
SINGLE-STAGE-TO-ORIBIT - A STEP CLOSER
Authors: FREEMAN DC STANLEY DO CAMARDA CJ LEPSCH RA COOK SA
Citation: Dc. Freeman et al., SINGLE-STAGE-TO-ORIBIT - A STEP CLOSER, Acta astronautica, 37, 1995, pp. 87-94
COMPARISON OF 2 MULTIDISCIPLINARY OPTIMIZATION STRATEGIES FOR LAUNCH-VEHICLE DESIGN
Authors: BRAUN RD POWELL RW LEPSCH RA STANLEY DO KROO IM
Citation: Rd. Braun et al., COMPARISON OF 2 MULTIDISCIPLINARY OPTIMIZATION STRATEGIES FOR LAUNCH-VEHICLE DESIGN, Journal of spacecraft and rockets, 32(3), 1995, pp. 404-410
DUAL-FUEL PROPULSION IN SINGLE-STAGE ADVANCED MANNED LAUNCH SYSTEM VEHICLE
Authors: LEPSCH RA STANLEY DO UNAL R
Citation: Ra. Lepsch et al., DUAL-FUEL PROPULSION IN SINGLE-STAGE ADVANCED MANNED LAUNCH SYSTEM VEHICLE, Journal of spacecraft and rockets, 32(3), 1995, pp. 417-425
DESIGN OPTIONS FOR ADVANCED MANNED LAUNCH SYSTEMS
Authors: FREEMAN DC TALAY TA STANLEY DO LEPSCH RA WILHITE AW
Citation: Dc. Freeman et al., DESIGN OPTIONS FOR ADVANCED MANNED LAUNCH SYSTEMS, Journal of spacecraft and rockets, 32(2), 1995, pp. 241-249
ROCKET-POWERED SINGLE-STAGE VEHICLE CONFIGURATION SELECTION AND DESIGN
Authors: STANLEY DO ENGELUND WC LEPSCH RA MCMILLIN M WURSTER KE POWELL RW GUINTA T UNAL R
Citation: Do. Stanley et al., ROCKET-POWERED SINGLE-STAGE VEHICLE CONFIGURATION SELECTION AND DESIGN, Journal of spacecraft and rockets, 31(5), 1994, pp. 792-798
TECHNOLOGY AND STAGING EFFECTS ON 2-STAGE-TO-ORBIT SYSTEMS
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
WINGED BOOSTER PERFORMANCE WITH COMBINED ROCKET AND AIRBREATHING PROPULSION
Authors: LEPSCH RA NAFTEL JC
Citation: Ra. Lepsch et Jc. Naftel, WINGED BOOSTER PERFORMANCE WITH COMBINED ROCKET AND AIRBREATHING PROPULSION, Journal of spacecraft and rockets, 30(6), 1993, pp. 641-646
Risultati: 1-7 |