martinbayer
ACCESS: Above Top Secret
- Joined
- 6 January 2009
- Messages
- 5,081
- Reaction score
- 6,994
I was never directly involved in any asymmetrical TSTO RLV studies (horror & heresy!) at Boeing, or any of my other previous German employers for that matter, but I was aware of some related work at Boeing - I always thought of it as some kind of Hunchback of Notre Dame like travesty...The asymmetrical bimese (I KNOW it's an oxymoron) was a pretty good idea, by the way. Go ask @martinbayer
I did some random calculations, with 460 seconds isp the two stages can have relatively low propellant mass fractions (0.80 or lower) and still deliver a payload. Well btw that was the Shuttle circa 1969, before the OMB cuts.