Investigation of liquid gun propellants : electrical ignition of LGP 1846KLINGENBERG, G; ROCKSTROH, H; KNAPTON, J. D et al.Propellants, explosives, pyrotechnics. 1990, Vol 15, Num 3, pp 103-114, issn 0721-3115, 12 p.Article

ATTITUDES OF THE ANTARCTIC SOUNDING ROCKET VEHICLESTOHYAMA F; AOYAMA I.1978; MEM. NATION. INST. POLAR RES., SPEC. ISSUE; JPN; DA. 1978; NO 9; PP. 87-91Conference Paper

AIAA SOUNDING ROCKET TECHNOLOGY CONFERENCE. 4. PROCEEDINGS; BOSTON, MASS.; 1976.1976; ; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. (308P.); BIBL. DISSEM.Conference Paper

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Steady-state high pressure LOx/H2 rocket engine combustionSMITH, Joshua J; SCHNEIDER, Gerald; SUSLOV, Dmitry et al.Aerospace science and technology. 2007, Vol 11, Num 1, pp 39-47, issn 1270-9638, 9 p.Conference Paper

Rocket Plume ModelingCHUNPEI CAI.AIAA journal. 2014, Vol 52, Num 12, pp 2907-2910, issn 0001-1452, 4 p.Article

Méthodologie de dimensionnement des ensembles propulsifs = Methodology of the design of cryogenic liquid propellant rocket enginesAkichi, Agboué; Noguèra, R.1994, 148 p.Thesis

Comparison of predictions based on three control volume models of subsonic/supersonic ejector systemsKREMAR, J; PEDDIESON, J; HAN, S et al.Acta mechanica. 2007, Vol 193, Num 1-2, pp 85-99, issn 0001-5970, 15 p.Article

On the computation of ionization levels in rocket exhaust flamesCOUSINS, J. M; JENSEN, D. E.Combustion and flame. 1983, Vol 52, Num 2, pp 111-125, issn 0010-2180Article

Projectile impact ignition characteristics of propellants. III: Effect of particle size and porosityANDERSEN, W. H; STILLMAN, G. P.Combustion science and technology. 1983, Vol 32, Num 5/6, pp 237-244, issn 0010-2202Article

The determination and analysis of the orbit of NIMBUS 1 ROCKET, 1964-52B. II: Variations in orbital eccentricityBOULTON, W. J.Planetary and space science. 1985, Vol 33, Num 6, pp 735-756, issn 0032-0633Article

Variable structure control of time-delay systems with a simulation study on stabilizing combustion in liquid propellant rocket motorsFENG ZHENG; MIAN CHENG; WEI-BING GAO et al.Automatica (Oxford). 1995, Vol 31, Num 7, pp 1031-1037, issn 0005-1098Article

Die Erdrakete als Sonde = The earth rocket as a probeGUDEHUS, G.BMT. Baumaschine + Bautechnik. 1993, Num 3, pp 129-134, issn 0005-6693Article

Damage-mitigating control of a reusable rocket engine : Part I-Life prediction of the main thrust chamber wallDAI, X; RAY, A.Journal of dynamic systems, measurement, and control. 1996, Vol 118, Num 3, pp 401-408, issn 0022-0434Article

Theoretical analysis of hydrides in solid and hybrid rocket propulsionMAGGI, Filippo; GARIANI, Gabriela; GALFETTI, Luciano et al.International journal of hydrogen energy. 2012, Vol 37, Num 2, pp 1760-1769, issn 0360-3199, 10 p.Article

Experimental investigation of liquid helium pressurization method for liquid propellant rocketIN, Sehwan; JEONG, Sangkwon; KIM, Youngkwon et al.JSME international journal. Series B, fluids and thermal engineering. 2005, Vol 48, Num 2, pp 300-304, issn 1340-8054, 5 p.Conference Paper

La Chine, nouvelle puissance spatialeSOTTY, Christian.La Recherche (Imprimé). 2012, Num 469, pp 72-74, issn 0029-5671, 3 p.Article

Fra Leipzig til London or From Leipzig to London: a translation from the danishCLYENS, S; JOHNSON, W.International journal of impact engineering. 1995, Vol 16, Num 1, pp 171-184, issn 0734-743XArticle

SensitivityKayaku Gakkaishi. 1996, Vol 57, Num 1, issn 1340-2781, 49 p.Serial Issue

Oscillations of a rotary fluid flowing out of a closed vesselORLOV, V. V; TEMNOV, A. N.Journal of engineering physics and thermophysics. 2000, Vol 73, Num 1, pp 165-174, issn 1062-0125Article

Vinci: Un moteur rallumable pour Ariane 5 = Vinci, the Re-ignitable engine for Ariane 5Technologies France (Strasbourg). 1999, Num 58, pp 12-13, issn 1257-2489, 36 [3 p.]Article

Central spatial Ela 3 de Kourou (Guyane, 1991) = Ela 3 space centre of Kourou (Guiana, 1991)Travaux (Paris). 1992, Num 672, pp 70-71, issn 0041-1906Article

Modèle transitoire de combustion d'un propergol composé de mousse de polyurethane chargée en octogene = Transitory model of combustion of a propellant composed of polyurethane foam charged with octogenGALANT, S; GROUSET, D; REBUFFAT, D et al.Lecture notes in physics. 1985, Vol 241, pp 251-266, issn 0075-8450Article

Experimental study of the role of gas-liquid scheme injector as an acoustic resonator in a combustion chamberKIM, Haksoon; CHAE HOON SOHN.Journal of mechanical science and technology. 2006, Vol 20, Num 6, pp 896-904, issn 1738-494X, 9 p.Article

Performance of a Titan rocket engine using laser-induced fluorescence of OHCOHEN, L. M; JASSOWSKI, D. M; ITO, J. I et al.AIAA journal. 2001, Vol 39, Num 10, pp 1926-1935, issn 0001-1452Conference Paper