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Izvoz spreman — 
Slika omota

Fundamentals of hybrid rocket combustion and propulsion /

Spremljeno u:
Bibliografski detalji
Daljnji autori: Chiaverini, Martin J. (Martin John), 1968-, Kuo, Kenneth K.
Format: Knjiga
Jezik:engleski
Published: Reston, Va. : American Institute of Aeronautics and Astronautics, [2007], ©2007.
Serija:Progress in astronautics and aeronautics ; v. 218.
Teme:
Hybrid propellant rockets.
Rocket engines > Combustion.
Rockets (Aeronautics) > Fuel.
Rocket engines.
Rockets (Aeronautics)
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Annex

Detalji primjeraka od Annex
Signatura: TL 783.45 .F96 2007
Dostupno Postavi narudžbu Request a scan of an article or book chapter

Slični predmeti

  • Liquid rocket thrust chambers : aspects of modeling, analysis, and design
    Izdano: (2004)
  • Liquid propellant rocket combustion instability
    od: Harrje, David T., i dr.
    Izdano: (1972)
  • Liquid hydrogen as a propulsion fuel, 1945-1959
    od: Sloop, John L.
    Izdano: (1978)
  • Design of liquid propellant rocket engines
    od: Huzel, Dieter K., i dr.
    Izdano: (1971)
  • Vibration, acoustic, and shock design and test criteria for components on the solid rocket boosters (SRB), lightweight external tank (LWT), and space shuttle main engines (SSME)
    Izdano: (1984)

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