SSTO_vs_TSTO_for_LEO_Mission.tif
Size of this JPG preview of this TIF file:
800 × 582 pixels
.
Other resolutions:
320 × 233 pixels
|
640 × 466 pixels
|
914 × 665 pixels
.
Summary
Description SSTO vs TSTO for LEO Mission.tif |
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 |
Licensing
I, the copyright holder of this work, hereby publish it under the following license:
This file is licensed under the
Creative Commons
Attribution-Share Alike 4.0 International
license.
-
You are free:
- to share – to copy, distribute and transmit the work
- to remix – to adapt the work
-
Under the following conditions:
- attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
- share alike – If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.