On the detectability of several varieties of low-energy starshipsMATLOFF, G. L.JBIS. Journal of the British Interplanetary Society. 1994, Vol 47, Num 1, pp 17-18, issn 0007-084XArticle

Linearized impulsive rendezvous problemCARTER, T. E; BRIENT, J.Journal of optimization theory and applications. 1995, Vol 86, Num 3, pp 553-584, issn 0022-3239Article

Dynamics of an orbital dual-spin film systemGULYAEV, V. I; GROM, A. A; KOSHKIN, V. L et al.International applied mechanics. 1993, Vol 29, Num 5, pp 406-411, issn 1063-7095Article

Prestrssing a space structureKWAN, A. S. K; PELLEGRINO, S.AIAA journal. 1993, Vol 31, Num 10, pp 1961-1963, issn 0001-1452Article

On the analysis of the motion of a class of mechanical systems with a discontinuous nonhomogeneityZHECHEV, M. M; KHOROSHILOV, V. S.International applied mechanics. 1993, Vol 29, Num 3, pp 239-241, issn 1063-7095Article

On the permanent rotation of a torque-free two-body system with a flexible connectionLIU, Y. Z; RIMROTT, F. P. J.Journal of applied mechanics. 1994, Vol 61, Num 1, pp 199-202, issn 0021-8936Article

Simple mathematical models of the explosive failure of a spacecraftKISELEV, A. B.Journal of applied mechanics and technical physics. 1995, Vol 36, Num 2, pp 287-293, issn 0021-8944Article

Optical processing for semiautonomous terminal navigation and dockingSCHOLL, M. S.Applied optics. 1993, Vol 32, Num 26, pp 5049-5055, issn 0003-6935Article

THE OPERATIONAL PERFORMANCE OF REENTRY VEHICLE HEATSHIELD THERMODYNAMIC INSTRUMENTATION = PERFORMANCES OPERATIONNELLES DES APPAREILS DE MESURE THERMODYNAMIQUE DES ECRANS THERMIQUES DES VEHICULES SPATIAUX RECUPERABLESLEGENDRE PJ; CHASE GT JR.1974; I.S.A. TRANS.; U.S.A.; DA. 1974; VOL. 13; NO 2; PP. 132-141; BIBL. 18 REF.Article

THERMAL CONTROL DESIGN AND ANALYSIS OF NAVIGATION TECHNOLOGY SATELLITE I. = CONCEPTION ET ANALYSE DE LA REGULATION DE TEMPERATURE DU NAVIGATION TECHNOLOGY SATELLITE I (NTS-I)HWANGBO H; ROVINSKI RS; FISKUM RJ et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. 10TH THERMOPHYS. CONF.; DENVER, COLO.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 655; PP. 1-7; BIBL. 4 REF.Conference Paper

Structural sensor testing for space vehicle applicationsHUANG, Jerry; ROSE, John; GORDON, Jason et al.SPIE proceedings series. 2005, pp 88-99, isbn 0-8194-5743-4, 12 p.Conference Paper

Modeling of Electron Energy Phenomena in Hypersonic FlowsKIM, Minkwan; GÜLHAN, Ali; BOYD, Iain D et al.Journal of thermophysics and heat transfer. 2012, Vol 26, Num 2, pp 244-257, issn 0887-8722, 14 p.Article

The scheme of satellite navigation performance evaluation and test system based on simulationXIAOJING XIA; DONG XU; YAN ZHAO et al.Proceedings of SPIE, the International Society for Optical Engineering. 2008, Vol 7128, pp 71282S.1-71282S.5, issn 0277-786X, isbn 978-0-8194-7362-2 0-8194-7362-6Conference Paper

Mass spectrometric investigation of high enthalpy plasma flowsSCHÖNEMANN, A; AUWETER-KURTZ, M.Journal of thermophysics and heat transfer. 1995, Vol 9, Num 4, pp 620-628, issn 0887-8722Article

Characteristics of a high-enthalpy electric-arc heater for air at atmospheric pressureSERGEEV, V. L.Journal of engineering physics and thermophysics. 1994, Vol 66, Num 5, pp 524-533, issn 1062-0125Article

Program motion of systems or rigid and elastic bodies (review)ZAKRZHEVSKII, A. E.International applied mechanics. 1993, Vol 29, Num 6, pp 413-430, issn 1063-7095Article

Modeling, simulation, and verification of space-based systems II (31 March 2005, Orlando, Florida, USA)Motaghedi, Pejmun.Proceedings of SPIE, the International Society for Optical Engineering. 2005, issn 0277-786X, isbn 0-8194-5784-1, 1Vol, V-158 p, isbn 0-8194-5784-1Conference Proceedings

Radiative transfer in some aeronautical and aerospace devicesSOUFIANI, A.International heat transfer conference. 2002, pp 27-40, isbn 2-84299-308-X, 14 p.Conference Paper

An exact solution to the fuel optimal propulsive control of a tutorial structureREDMOND, J; SILVERBERG, L.Journal of sound and vibration. 1994, Vol 171, Num 1, pp 23-33, issn 0022-460XArticle

Dynamics and stabilization of a flexible orbiting spacecraft with a rigid tip bodyZHENG-HUA LUO; SAKAWA, Y.International journal of systems science. 1994, Vol 25, Num 2, pp 205-223, issn 0020-7721Article

Residual flexibility test method for verification of constrained structural modelsADMIRE, J. R; TINKER, M. L; IVEY, E. W et al.AIAA journal. 1994, Vol 32, Num 1, pp 170-175, issn 0001-1452Conference Paper

A general formulation for the nonlinear dynamics and control of orbiting flexible structuresMODI, V. J; NG, A. C; KARRAY, F et al.Computational mechanics. 1993, Vol 13, Num 3, pp 204-230, issn 0178-7675Article

MICROBIOLOGICAL SAMPLING OF THE SPACECRAFT ATMOSPHERE DURING A SIMULATED SKYLAB MISSION = PRELEVEMENT MICROBIOLOGIQUE DE L'ATMOSPHERE DU VAISSEAU SPATIAL AU COURS D'UNE MISSION SKYLAB SIMULEEBROCKETT RM; FERGUSON JK.1975; AVIAT. SPACE ENVIRONMENT. MED.; U.S.A.; DA. 1975; VOL. 46; NO 1; PP. 30-32; BIBL. 10REF.Article

MASS SPECTROMETERS FOR ATMOSPHERIC MONITORING AND CONTROL IN THE SHUTTLE ERA = SPECTROMETRES DE MASSE POUR LA SURVEILLANCE ET LE CONTROLE DE L'ATMOSPHERE A L'ERE DE LA NAVETTE SPATIALERUECKER MR; SHAVER FA.1974; IN: AM. SOC. MECH. ENG. INTERSOC. CONF. ENVIRON. SYST.; SEATTLE; 1974; NEW YORK; A.S.M.E.; DA. 1974; VOL. 20; PP. 1-17; BIBL. 14 REF.Conference Paper

OPTIMAL ANGULAR VELOCITY CONTROL WITH FINITE TERMINAL TIME FOR AN ASYMMETRIC SPACECRAFT. = COMMANDE OPTIMALE DE LA VITESSE ANGULAIRE POUR UN VEHICULE SPATIAL ASYMMETRIQUE EN HORIZON FINICOUPE GM.1974; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1974; VOL. 19; NO 5; PP. 582-583; BIBL. 3 REF.Article