File:SSTO vs TSTO for LEO Mission.tif

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English: Comparison of growth factor sensitivity for Single-Stage-to-Orbit (SSTO) and restricted stage Two-Stage-to-Orbit (TSTO) vehicle. Based on a LEO mission profile of delta v = 9.1 km/s and payload mass = 4500 kg for range of propellant Isp.
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Author Bernstein22

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Date/TimeThumbnailDimensionsUserComment
current21:29, 13 September 2014Thumbnail for version as of 21:29, 13 September 2014914 × 665 (125 KB)Bernstein22 (talk | contribs)increased resolution
20:20, 13 September 2014Thumbnail for version as of 20:20, 13 September 20141,502 × 1,090 (748 KB)Bernstein22 (talk | contribs)User created page with UploadWizard

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