Comment on Space Plane from The Next Shuttle

Greatings All, The story from

formatting link
if it rings true would prove a RLV does work. In The Next shuttle I go into the details of the LACES system that is likely the propulsion sytem.

It comes down to how much weight you have to takeoff / launch with. Liquid O2 is about 64 pounds per ft^3, where asw liquid hydrogen is on

4 pouns per ft^3. So you take off with only LH2.

You then while flying take a portion of hte turbine compressor air and put it in a liquid hdrogen cooled heat exchanger. Presto liquid air. you then centerfugge the N2 contenbt out and you gt 90% pure LOX. Andrews Space and TEchnology did a TSTO design in the mid 1990's and it was impressive: GTOW (gross takeoff weight : 800,000 , a bit bigger than a 747. Orbiter payload was 25,000 pounds. Scale this down a bit and you have a likely design for this SR-71 replacement with a

1-2 man crewed recon craft.

As a weapons payload a mass travrling at over 7000 feet/sec needs no explosive and would drill into any hardened target. It would get though the atmosphere in 20-25 seconds. And the orbiter would reach any point on Earth in 90 minutes. No wonder the military likes this.

As a RLV its a bit on the small side, but proves that it can be done.

And in other news folks, Space X is making a space capsule called Dracoon. At about 3.5 meters in diameter and to service the ISS. It will launch on top of a Falcon 9 booster. Lets hope Space X can make it fly . IT will be flying by 2009. t/Space wont be ready by then. in my humble opion.

Reply to
RocketEngineer
Loading thread data ...

PolyTech Forum website is not affiliated with any of the manufacturers or service providers discussed here. All logos and trade names are the property of their respective owners.