question on hyrdogen launchers



Consider the result of a decision that the fuel for the launcher must be
LH2. Given the necessary size due to the low density of LH2, is there a
point beyond which additional fuel is more than offset by the need for
additional support structure? How do things scale?

That is, is there in principal a maximum mass that can be launched with
LH2/LO2?

--
ciao,
Bruce

drift wave turbulence: http://www.rzg.mpg.de/~bds/

.



Relevant Pages

  • Re: question on hyrdogen launchers
    ... Given the necessary size due to the low density of LH2, is there a point beyond which additional fuel is more than offset by the need for additional support structure? ... Once in orbit, reentry is accomplished rather simply, as the dynamic load on any square foot of the tankage is immensely low, it will float back to the atmosphere like a big balloon. ...
    (sci.space.policy)
  • Re: question on hyrdogen launchers
    ... > Consider the result of a decision that the fuel for the launcher must be ... > LH2. ... Given the necessary size due to the low density of LH2, ...
    (sci.space.policy)
  • Re: question on hyrdogen launchers
    ... > Consider the result of a decision that the fuel for the launcher must be ... > LH2. ... orbit would likely require significant RCS just to keep it in orbit. ...
    (sci.space.policy)
  • Re: "Two events" on ascent
    ... this should help kill any future use of liquid hydrogen ... >> fuel in a new launcher. ... Perhaps one of the un-plonked could ask Dr. Duck why he likes LH2. ... Or maybe he's thinking that a completely re-useable launcher is ...
    (sci.space.shuttle)
  • Re: Hydrogen Cars, Trucks, and Buses Are the Answer Indeed
    ... Force liquid hydrogen (LH2) fuel project. ... aircraft being developed ... including Kelly Johnson and the others you mention which is WHY he said ...
    (sci.energy.hydrogen)

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