Abstract
Liquid hydrogen appears to be a very attractive propeilant either in chemical systems in which it is burned with an oxidant, or as monopropellant when it is heated by some device like a nuclear reactor. Its low atomic weight, high specific heat and high heat of combustion all contribute to high specific-impulse values for either of the two propulsion systems. The undesirable characteristics of the propeilant include a large specific volume and difficult handling procedure for a low-temperature cryogen.
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Graham, R.W., Hendricks, R.C., Hsu, Y.Y., Friedman, R. (1961). Experimental Heat Transfer and Pressure Drop of Film Boiling Liquid Hydrogen Flowing Through a Heated Tube. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 6. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0534-8_54
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DOI: https://doi.org/10.1007/978-1-4757-0534-8_54
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