File:SSTO vs TSTO for LEO Mission.tif
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Summary
| Description |
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. |
| Date | |
| Source | Own work |
| Author | Bernstein22 |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 21:29, 13 September 2014 |  | 914 × 665 (125 KB) | Bernstein22 | increased resolution |
| 20:20, 13 September 2014 |  | 1,502 × 1,090 (748 KB) | Bernstein22 | User created page with UploadWizard |
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