I made a rather crude Python script to generate a Glideslope.cfg entry for a base:
https://pastebin.com/tr5euFqM
I'm not too confident trying to overwrite people's .cfg files so have left the user to do some copying and pasting.
Usage:
1. Copy contents of the entire base file (e.g...
In Orbiter I can reach a Moron-TAL with one engine out from launch, and an ATO shortly after. This is with a payload set to 25 tonnes.
Clearly either the real life abort windows are rather conservative, or the simulated characteristics in Orbiter are a bit generous, does anyone know which?
I think this is relevant enough to revive the thread:-
I have put this soundtrack over an Orbiter scenario to show (approximately) what would be going on.
Challenge 1 (Launch and Dock): 5927.23 kg used
Challenge 2 (Earth-Luna OB1): 2579.04 kg used
Challenge 3 (Earth-Luna OB1): 3338.85 kg used
Challenge 4 (Reentry): 387.5 kg used (0 kg main / 3.7 kg RCS remaining)
This site uses cookies to help personalise content, tailor your experience and to keep you logged in if you register.
By continuing to use this site, you are consenting to our use of cookies.