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Volumn , Issue , 1999, Pages

Development of a pressure-fed rocket engine using hydrogen peroxide and JP-8

Author keywords

[No Author keywords available]

Indexed keywords

CATALYSTS; CHEMICAL REACTIONS; COMBUSTION CHAMBERS; EROSION; FLAMMABILITY TESTING; FUELS; HYDROGEN PEROXIDE; OXIDATION; PEROXIDES; PROPULSION; ROCKET ENGINES; ROCKETS;

EID: 59949100804     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (19)
  • 1
    • 0008944769 scopus 로고
    • Advantage of Hydrogen Peroxide as A Rocket Oxidant
    • Andrews, D., “Advantage of Hydrogen Peroxide as A Rocket Oxidant, ” Journal of The British Interplanetary Society, Vol.43, No. 7, 1990, p. 319-328.
    • (1990) Journal of the British Interplanetary Society , vol.43 , Issue.7 , pp. 319-328
    • Andrews, D.1
  • 3
    • 85003260272 scopus 로고
    • Hydrogen Peroxide as an Alternate Oxidizer for a Hybrid Rocket Booster
    • Ventura, M. C. and Heisfer, S. D., “Hydrogen Peroxide as an Alternate Oxidizer for a Hybrid Rocket Booster, ” Journal of Propulsion and Power, Vol. 11, No. 3, 1995, p. 562-565.
    • (1995) Journal of Propulsion and Power , vol.11 , Issue.3 , pp. 562-565
    • Ventura, M.C.1    Heisfer, S.D.2
  • 5
    • 84963886576 scopus 로고
    • Super Sprite, Jet Propulsion
    • “Super Sprite, ” Jet Propulsion, Journal of the American Rocket Society, Vol. 26, No. 3, 1956, p. 193.
    • (1956) Journal of the American Rocket Society , vol.26 , Issue.3 , pp. 193
  • 6
    • 84963892160 scopus 로고
    • Hydrogen Peroxide Handbooks AFRPL-TR-67-144, Air Force Rocket Propulsion Laboratory, Edwards Air Force Base, CA
    • Hydrogen Peroxide Handbooks AFRPL-TR-67-144, Air Force Rocket Propulsion Laboratory, Edwards Air Force Base, CA, 1967.
    • (1967)
  • 13
    • 0017547138 scopus 로고
    • Penetration and Breakup of Liquids in Subsonic Airstreams
    • Schetz, J. A. and Padhye, A., “Penetration and Breakup of Liquids in Subsonic Airstreams, ” AIAA Journal, Vol. 15, No. 10, 1977, p. 1385-1390.
    • (1977) AIAA Journal , vol.15 , Issue.10 , pp. 1385-1390
    • Schetz, J.A.1    Padhye, A.2
  • 14
    • 0032025965 scopus 로고    scopus 로고
    • Spray Structures of Liquid Jets Atomized in Subsonic Crossflows
    • Wu, P.-K., Kirkendall, K. A., Fuller, R. P., and Nejad, A. S., “Spray Structures of Liquid Jets Atomized in Subsonic Crossflows, ” Journal of Propulsion and Power, Vol. 14, No. 2, 1998, p. 173-182.
    • (1998) Journal of Propulsion and Power , vol.14 , Issue.2 , pp. 173-182
    • Wu, P.-K.1    Kirkendall, K.A.2    Fuller, R.P.3    Nejad, A.S.4
  • 15
    • 84963798733 scopus 로고    scopus 로고
    • Effects of Injection Angle on Liquid Jet Breakup in Subsonic Crossflow
    • Fuller, R. P., Wu, P.-K., Kirkendall, K. A., and Nejad, A. S., “Effects of Injection Angle on Liquid Jet Breakup in Subsonic Crossflow, ” AIAA Journal, in press, 1999.
    • (1999) AIAA Journal
    • Fuller, R.P.1    Wu, P.-K.2    Kirkendall, K.A.3    Nejad, A.S.4
  • 16
  • 17
    • 19644383154 scopus 로고
    • Impinging Jet Injector Atomization
    • Yang, V., and Anderson, W. E., Progress in Astronautics and Aeronautics
    • Anderson, W. E., Ryan, H. M., and Santoro, R.J., “Impinging Jet Injector Atomization, ” Liquid Rocket Engine Combustion Instability, ed. By Yang, V., and Anderson, W. E., Progress in Astronautics and Aeronautics, Vol. 169, 1995, p. 215-246.
    • (1995) Liquid Rocket Engine Combustion Instability , vol.169 , pp. 215-246
    • Anderson, W.E.1    Ryan, H.M.2    Santoro, R.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.