![]() |
#1
|
|||
|
|||
![]()
Workable? Or just another flight of fancy?
"This airship flies from the upper atmospheric station to orbit. It uses hybrid chemical/electric propulsion to slowly accelerate and reach orbit. "A two mile wide station parked at 140,000 feet is the new way station to space. The station acts not only as a port for the orbital airship but also as a research center, construction site and tourist destination." See: http://www.jpaerospace.com/atohandout.pdf & https://www.thedrive.com/the-war-zon...spaces-founder |
#3
|
|||
|
|||
![]()
On 05-Jul-20 8:29 am, wrote:
Workable? Or just another flight of fancy? "This airship flies from the upper atmospheric station to orbit. It uses hybrid chemical/electric propulsion to slowly accelerate and reach orbit. "A two mile wide station parked at 140,000 feet is the new way station to space. The station acts not only as a port for the orbital airship but also as a research center, construction site and tourist destination." See: http://www.jpaerospace.com/atohandout.pdf & https://www.thedrive.com/the-war-zon...spaces-founder Would need to see some numbers for this. Will it actually be able to rise to 200,000 feet using buoyancy? More questionable, is whether it is possible to accelerate such a body to orbital speed using low thrust. As its speed rises, so will its altitude, but also so will the drag from the residual atmosphere. It is far from clear that it can achieve orbit that way. Sylvia. |
#4
|
|||
|
|||
![]()
On 2020-07-05 6:04 PM, JF Mezei wrote:
On 2020-07-04 20:14, Sylvia Else wrote: Will it actually be able to rise to 200,000 feet using buoyancy? More questionable, is whether it is possible to accelerate such a body to orbital speed using low thrust. As its speed rises, so will its altitude, but also so will the drag from the residual atmosphere. It is far from clear that it can achieve orbit that way. Isn't it more likely that the ship would be dropped from the balloon and ignite rockets to quickly accelerate to orbital speed before it falls down to the ground? And how do you get back down without a TPS? Or are you only interested in a one-way trip? You should read over the documentation a little more carefully. It seems clear the "orbiter" part of the design is also a balloon in a wedge shape. That is to allow for *gradual* descent back into the atmosphere without having to worry about lift and control vs heating during descent. It's interesting tho, I didn't see how the engine configuration as drawn shows how that's possible unless the engines have reversible thrust. The balloon wedge geometry would be wrong if you inverted the craft for decent. [snip] Would be interesting for aircraft design though with regards to Max-Q. I agree with the latter. This is the slow path to/from orbit. Dave |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Venus Airships / by Brad Guth | BradGuth | History | 105 | August 10th 08 06:00 AM |
The Great Airships of 1897! | Double-A | Misc | 28 | July 13th 06 02:44 AM |
an efficient orbit to fly a space craft from the L1 lagrange point from earth to mars sun-synchronous orbit? | kelvin | Space Shuttle | 1 | November 11th 05 03:21 AM |
An efficient orbit to fly a space craft from the L1 lagrange point to mars sun-synchronous orbit? | kelvin | Technology | 2 | November 10th 05 08:01 PM |
Orbit Data of the Optical Inter-orbit Communications Engineering Test Satellite | Jacques van Oene | News | 0 | August 24th 05 01:25 PM |