The ratio initial mass/payload mass - How good are launch systems?

Details The ratio initial mass/payload mass - How good are launch systems? The ratio initial mass/payload mass - How good are launch systems?

Apr 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992lr.....12...34h&link_type=abstract

Luft- und Raumfahrt (ISSN 0173-6264), vol. 12, no. 2, Mar.-Apr. 1992, p. 34, 36, 37. In German.

Computer Science

Performance

Payload Mass Ratio, Space Transportation, Spacecraft Performance, Propellant Mass Ratio, Reusable Spacecraft

Scientific paper

The growth factor G, defined as the ratio of initial mass/payload mass, is used here to evaluate various rocket launch systems. The qualities of the propulsion, structure, environmental loading, and costs of the Saturn 5, Space Shuttle, Titan III, Saenger Horus C and M, and various Ariane rockets are assessed. The results are used to evaluate the reusability of these propulsion systems.

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