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Results: 1-10 |
Results: 10
HYPERSONIC THERMAL ENVIRONMENT OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE
Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA RILEY CJ HAMILTON HH
Citation: Kj. Weilmuenster et al., HYPERSONIC THERMAL ENVIRONMENT OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE, Journal of spacecraft and rockets, 34(6), 1997, pp. 697-704
HYPERSONIC AERODYNAMIC CHARACTERISTICS OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE
Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA RILEY CJ HAMILTON HH ALTER SJ
Citation: Kj. Weilmuenster et al., HYPERSONIC AERODYNAMIC CHARACTERISTICS OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE, Journal of spacecraft and rockets, 33(4), 1996, pp. 463-469
INFLUENCE OF SONIC-LINE LOCATION ON MARS PATHFINDER PROBE AEROTHERMODYNAMICS
Authors: GNOFFO PA WEILMUENSTER KJ BRAUN RD CRUZ CI
Citation: Pa. Gnoffo et al., INFLUENCE OF SONIC-LINE LOCATION ON MARS PATHFINDER PROBE AEROTHERMODYNAMICS, Journal of spacecraft and rockets, 33(2), 1996, pp. 169-177
MARS PATHFINDER 6-DEGREE-OF-FREEDOM ENTRY ANALYSIS
Authors: BRAUN RD POWELL RW ENGELUND TC GNOFFO PA WEILMUENSTER KJ MITCHELTREE RA
Citation: Rd. Braun et al., MARS PATHFINDER 6-DEGREE-OF-FREEDOM ENTRY ANALYSIS, Journal of spacecraft and rockets, 32(6), 1995, pp. 993-1000
EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF SHUTTLE ORBITER HYPERSONICTRIM ANOMALY
Authors: BRAUCKMANN GJ PAULSON JW WEILMUENSTER KJ
Citation: Gj. Brauckmann et al., EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF SHUTTLE ORBITER HYPERSONICTRIM ANOMALY, Journal of spacecraft and rockets, 32(5), 1995, pp. 758-764
NAVIER-STOKES SIMULATIONS OF ORBITER AERODYNAMIC CHARACTERISTICS INCLUDING PITCH TRIM AND BODYFLAP
Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA
Citation: Kj. Weilmuenster et al., NAVIER-STOKES SIMULATIONS OF ORBITER AERODYNAMIC CHARACTERISTICS INCLUDING PITCH TRIM AND BODYFLAP, Journal of spacecraft and rockets, 31(3), 1994, pp. 355-366
MULTIBLOCK ANALYSIS FOR SHUTTLE ORBITER REENTRY HEATING FROM MACH 24 TO MACH 12
Authors: GNOFFO PA WEILMUENSTER KJ
Citation: Pa. Gnoffo et Kj. Weilmuenster, MULTIBLOCK ANALYSIS FOR SHUTTLE ORBITER REENTRY HEATING FROM MACH 24 TO MACH 12, Journal of spacecraft and rockets, 31(3), 1994, pp. 367-377
CHARACTERISTICS OF THE SHUTTLE ORBITER LEESIDE FLOW DURING A REENTRY CONDITION
Authors: KLEB WL WEILMUENSTER KJ
Citation: Wl. Kleb et Kj. Weilmuenster, CHARACTERISTICS OF THE SHUTTLE ORBITER LEESIDE FLOW DURING A REENTRY CONDITION, Journal of spacecraft and rockets, 31(1), 1994, pp. 8-16
HL-20 COMPUTATIONAL FLUID-DYNAMICS ANALYSIS
Authors: WEILMUENSTER KJ GREENE FA
Citation: Kj. Weilmuenster et Fa. Greene, HL-20 COMPUTATIONAL FLUID-DYNAMICS ANALYSIS, Journal of spacecraft and rockets, 30(5), 1993, pp. 558-566
SOLUTION STRATEGY FOR 3-DIMENSIONAL CONFIGURATIONS AT HYPERSONIC SPEEDS
Authors: WEILMUENSTER KJ GNOFFO PA
Citation: Kj. Weilmuenster et Pa. Gnoffo, SOLUTION STRATEGY FOR 3-DIMENSIONAL CONFIGURATIONS AT HYPERSONIC SPEEDS, Journal of spacecraft and rockets, 30(4), 1993, pp. 385-394
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