I know..it would need to have detachable nose made of carbon to get it pressurized and a man in.
Perlan II has pressirization up to 90 000 ft and it is a glider.
Measures corrected !
SPECS INDICATED…AND 2 PASSENGERS.
Measures corrected !
Here are the basics in one man sized plane..quite a lot of punch for the weight still ?
It is a pusher prop with 2 x 10 kw engines….and uses 30-50% efficient solar panels ( top notch ).
What is ponzi anyway ?
Ah so se are still in the realms of fiction!!:)
Yes they are fiction…but so was Jules Verne about the moon voyage !
Intriguing. But the question is verging on the metaphysical. Why? might be a better question.
Nothing I suppose is the answer. Corusant??
Coruscant; http://starwars.wikia.com/wiki/Coruscant
Let’s reverse the question.
What would it take for you to believe there is a God ?
If we made a manned journey to Alfa Centauri and found out that Corusant actually exists there.
Would that please you and make you say…Moses was right…there is a ( judeo-christian ) God ?
I redrew the mother ship with 130 m spanning and 50 000 mtow to carry a tad bigger space ship into orbit.
BTW: Which Star Wars caracter are you ?
I was Obi-Wan.
http://www.zimbio.com/quiz/Ukldm8Pi5Ub/Star+Wars+Character/result/2nWJJiPNR1D
After some further converstions at two space flight site I have this for you;
I’ll do some math for you.
L=½pv^2ACl = > ½x0.0000009kg/m3x38098384x1290x3 = 66348 N ….witch means an object with cl3 flying at 140 km can weigh 6635 kilos ( with 1290 m2 wing area )…now check the centrifugal force in 140km….
12 700 kg (weight with empty fuel in Solar Eagle at 140 km) x a ( a= v^2/r ) = 12700×5.7 = 72843 N …..that means that the plane is forced into orbit with force of 72843 N ie 7284 kg can be reduced from the weight of 12700…so Solar Eagle with Star Eagle are still cimbing at 140 km !
The Solar Eagle can theoretically fly really near the LEO at 160 km altitude…making the space flite very economical since carrying a space ship capable to moon landing at 1/240th of the fuel used in APOLLO 11.
Tuned specs for weight and power here.
Tuned specs for weight and power here.
This sounds a bit strange…but I calculated that the ship has enough wing area and thrust when carrying a space craft with a rocket engine after flying to 25 km with solar power that it could hit 17 000 km/h at 120 km altitude.
Compared to Apollo mission it would save rocket fuel 11900 barrels per flight.
This sounds a bit strange…but I calculated that the ship has enough wing area and thrust when carrying a space craft with a rocket engine after flying to 25 km with solar power that it could hit 17 000 km/h at 120 km altitude.
Compared to Apollo mission it would save rocket fuel 11900 barrels per flight.
Here is some math to prove that a carrier can lift 17000 kg to 80 km.
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Here is how to define the speed of 8000 km/h for the craft at 80 km; http://en.wikipedia.org/wiki/K%C3%A1rm%C3%A1n_line
Take lift equation… ½ x p x v^2 x A x Cl = 0,5 x 0.0001846 kg/m3 x 4937777 m/s x 1200 m2 x 0,5 = 273454 N = ~27000 kg ( 1 % less gravity )
It says 27 000 kg ship doing 8000 km/h with 1200 m2 wing area stays airborne at 80 km when Cl is 0,5 !
Air densities; http://www.engineeringtoolbox.com/standard-atmosphere-d_604.html