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|    sci.space.tech    |    Technical and general issues related to    |    3,113 messages    |
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|    Message 2,296 of 3,113    |
|    th to Ilpo Lagerstedt    |
|    Re: LH2/LOX in the first stage    |
|    02 Jan 05 19:40:40    |
      From: someguy@somewhere.se.retro.com              Ilpo Lagerstedt wrote:       > Why not any first stage with LH2/LOX before Delta IV?       >       Depends on what you mean with first stage. The Shuttle main engines burn       H2/O2 since many years, Ariane5 does as well, but both these vehicles       use/need solid fuel boosters to do a proper lift-off. Note also that the       main engines ignite some seconds before the boosters are ignited in       order to give full thrust at lift-off.              How does the Delta IV work in this respect? Is there any specific       ignition order and how quickly do the engines give full thrust from       ignition?              --       th              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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