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Results:
1-9
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Results: 9
Authors:
ASHENBERG J
LORENZINI EC
Citation: J. Ashenberg et Ec. Lorenzini, DYNAMICS OF A DUAL-PROBE TETHERED SYSTEM, Journal of guidance, control, and dynamics, 20(6), 1997, pp. 1265-1268
Authors:
ASHENBERG J
LORENZINI EC
Citation: J. Ashenberg et Ec. Lorenzini, DYNAMICAL CHARACTERISTICS OF A TETHERED STABILIZED SATELLITE, Journal of guidance, control, and dynamics, 20(6), 1997, pp. 1268-1271
Authors:
ASHENBERG J
Citation: J. Ashenberg, SATELLITE PITCH DYNAMICS IN THE ELLIPTIC PROBLEM OF 3 BODIES, Journal of guidance, control, and dynamics, 19(1), 1996, pp. 68-74
Authors:
ASHENBERG J
Citation: J. Ashenberg, ON THE EFFECTS OF TIME-VARYING AERODYNAMICAL COEFFICIENTS ON SATELLITE ORBITS, Acta astronautica, 38(2), 1996, pp. 75-86
Authors:
ASHENBERG J
Citation: J. Ashenberg, VIRTUAL AERODYNAMICAL COEFFICIENTS OF A ROTATING SATELLITE, Journal of spacecraft and rockets, 33(4), 1996, pp. 594-596
Authors:
ASHENBERG J
BROUCKE RA
Citation: J. Ashenberg et Ra. Broucke, EFFECTS OF GENERAL ATMOSPHERIC PERTURBATIONS ON SMALL DEBRIS PARTICLEORBITS, Journal of spacecraft and rockets, 32(5), 1995, pp. 912-917
Authors:
ASHENBERG J
Citation: J. Ashenberg, PROPAGATION OF PARTICLES DUE TO AN EXPLOSION IN ELLIPTIC ORBIT, Journal of guidance, control, and dynamics, 17(3), 1994, pp. 629-630
Authors:
ASHENBERG J
Citation: J. Ashenberg, FORMULAS FOR THE PHASE CHARACTERISTICS IN THE PROBLEM OF LOW EARTH ORBITAL DEBRIS, Journal of spacecraft and rockets, 31(6), 1994, pp. 1044-1049
Authors:
ASHENBERG J
Citation: J. Ashenberg, PERTURBED VOLUME OF ORBITING DEBRIS, Journal of spacecraft and rockets, 31(3), 1994, pp. 526-528
Risultati:
1-9
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