Closed TheGLine closed 4 years ago
Mostly completed LKO payloads, need to test a few. Add GEO/GTO stats for those rockets which are specialised for it (e.g most of the Centaur variants)
LKO requirements (JNSQ) = >5000 dV with a reasonable TWR using KER as a guide. Something around >1.2 TWR for first 4k dV or so, then >0.6 for final 1k dV circulisation burn.
Potential sources of information for more "theoretical" calculations of payload-to-orbit calculations:
https://spacecraft.ssl.umd.edu/academics/791S16/791S16L03.rocket_perf.pdf http://silverbirdastronautics.com/LaunchMethodology.pdf