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Results 1 to 25 of 3311

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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

A collection of technical papers/AIAA sounding rocket conference, Orlando FL, October 26-28, 1982AIAA sounding rocket conference. 6. 1982, 325 p.Conference Proceedings

PropellantsKayaku Gakkaishi. 1996, Vol 57, Num 4, issn 1340-2781, 38 p.Serial Issue

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

The determination and analysis of the orbit of NIMBUS 1 ROCKET, 1964-52B. I: The orbitsBOULTON, W. J.Planetary and space science. 1985, Vol 33, Num 6, pp 721-734, issn 0032-0633Article

A review on hydrogen industrial aerospace applicationsCECERE, D; GIACOMAZZI, E; INGENITO, A et al.International journal of hydrogen energy. 2014, Vol 39, Num 20, pp 10731-10747, issn 0360-3199, 17 p.Article

Application of laser-induced fluorescence (LIF) to liquid-propellant rocket engine testingBRASIER, C. W; DRAKES, J. A; SIMMONS, M. A et al.AGARD conference proceedings. 1998, pp 28.1-28.10, issn 0549-7191, isbn 92-836-0055-XConference Paper

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

Bonding a HTPB liner to modern rocket case materialsSANDEN, R; WINGBORG, N.Journal of applied polymer science. 1989, Vol 37, Num 1, pp 167-171, issn 0021-8995Article

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

The Ariane projectLUTON, J.-M; SCHMITT, D.Fusion engineering and design. 1999, Vol 46, Num 2-4, pp 449-455, issn 0920-3796Conference Paper

PIT FORMATION ON THE ACCELERATED SOLID PROPELLANT COMBUSTION SURFACE.MITANI T.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 9; PP. 1338-1340; BIBL. 6 REF.Article

TRANSIENT PERIOD OF THE ACCELERATION-PRODUCED BURNING RATE AUGMENTATION.NIIOKA T; MITANI T; ISHII S et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 9; PP. 1165-1169; BIBL. 12 REF.Article

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

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