메뉴 건너뛰기




Volumn 4, Issue , 2007, Pages 3530-3539

Test facility development for the 15,000 lb thrust Peregrine hybrid sounding rocket

Author keywords

[No Author keywords available]

Indexed keywords

LIQUID FUELS; NASA; OXIDANTS; TEST FACILITIES; THRUST REVERSAL;

EID: 36749076021     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-5358     Document Type: Conference Paper
Times cited : (11)

References (6)
  • 1
    • 10244247750 scopus 로고    scopus 로고
    • Scale-Up Tests of High Regression Rate Paraffin-Based Hybrid Rocket Fuels
    • November-December
    • A. Karabeyoglu, et al. Scale-Up Tests of High Regression Rate Paraffin-Based Hybrid Rocket Fuels, AIAA Journal of Propulsion and Power, Vol. 20, No. 6, November-December 2004.
    • (2004) AIAA Journal of Propulsion and Power , vol.20 , Issue.6
    • Karabeyoglu, A.1
  • 2
    • 77956851904 scopus 로고    scopus 로고
    • Overview of a 4-Inch Paraffin-Based Hybrid Sounding Rocket Program
    • AIAA-2004-3822
    • D. Van Pelt, et al. Overview of a 4-Inch Paraffin-Based Hybrid Sounding Rocket Program, AIAA-2004-3822, Joint Propulsion Conference 2004.
    • (2004) Joint Propulsion Conference
    • Van Pelt, D.1
  • 3
    • 36749042375 scopus 로고    scopus 로고
    • Design and Development of a 100km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle
    • AIAA-2007-5362
    • J. Dyer, K. Lohner, E. Doran, Z. Dunn, et al. Design and Development of a 100km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle. AIAA-2007-5362, Joint Propulsion Conference, 2007.
    • (2007) Joint Propulsion Conference
    • Dyer, J.1    Lohner, K.2    Doran, E.3    Dunn, Z.4
  • 4
    • 36749086509 scopus 로고    scopus 로고
    • Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization
    • AIAA-2007-5352
    • E. Doran, K. Lohner, J. Dyer, Z. Dunn, et al. Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization. AIAA-2007-5352, Joint Propulsion Conference 2007.
    • (2007) Joint Propulsion Conference
    • Doran, E.1    Lohner, K.2    Dyer, J.3    Dunn, Z.4
  • 5
    • 34249034256 scopus 로고    scopus 로고
    • Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System
    • AIAA-2006-4671
    • K. Lohner, J. Dyer, E. Doran, Z. Dunn, G. Zilliac Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System, AIAA-2006-4671, Joint Propulsion Conference 2006.
    • (2006) Joint Propulsion Conference
    • Lohner, K.1    Dyer, J.2    Doran, E.3    Dunn, Z.4    Zilliac, G.5
  • 6
    • 84888670403 scopus 로고    scopus 로고
    • NASA/TM-2003-211864, National Aeronautics and Space Administration
    • G. Zilliac, et al. Ames Hybrid Combustion Facility, NASA/TM-2003-211864, National Aeronautics and Space Administration, 2003.
    • (2003) Ames Hybrid Combustion Facility
    • Zilliac, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.