Launching Spacecraft From Aircraft
Embedded Geek writes: "New Scientist has an article on a proposed launch scheme named 'Bladerunner' (presumably, someone is a P.K. Dick fan) that would
use a pneumatic launcher to shove a launch vehicle out the back of a military transport aircraft at high altitude (40,000 feet/12,000 meters). As with all the new systems (such as this one) the goal is to reduce launch costs to more reasonable levels (to about $6K/kilo from today's $11-44K). An existing Pegasus system uses dedicated B-52s with the vehicle slung underneath, but Bladerunner would be an improvement by not requiring dedicated planes (the launcher could be set up on a transport in 24 hours) and also could accomodate larger vehicles (since it wouldn't be slung underneath)."
The term "Bladerunner" is imho not a P.K.Dick-Term. The Story is entitled "Do Androids Dream Of Electric Sheep", the title "Bladerunner" was first used in the movie by R. Scott.
Can anyboy enlighten me where it is from?
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Could be worse. Could be raining.
How does the pilot of the launching aircraft deal with the huge changes in the center-of-gravity when a large missile (Pegasus XL weighs about 50,000 lbs) is ejected from the rear of the aircraft.
Mea navis aericumbens anguillis abundat
The space shuttle originally was supposed to operate this way, with one plane carrying the spacecraft part to high altitude and then rocketing from there. It was rejected because it required developing a big plane as well as the shuttle. This method may be an improvement over that proposal.
So long and thanks for all the fish . . . !!!
Price per kilo to orbit is NOT the only hurdle! I can see three major obstacles off the top of my head:
No Funding: Who in this age of recession is foolhardy enough to finance such a venture after all the venture capital firms got burned in last years crash?
Payload design: Modern satellites are custom designed to match their launchers. Diameter, mass, etc are optimized during the design stages to the specifications of the intended launcher. Who exactly is going to redesign their multi-million dollar satellites for the unique constraints used in this design?
Market: Who will be buying? Any air lauched design is going to be limited by the launch aircraft, in Pegasus's (L1011) case by aircraft's undercarriage, and in Bladerunner's (Which aircraft? C131/C5/C17's? Good luck in convincing the USAF to lend you one, they are waaay overtasked already.) by cargo bay weight constraints. Since Iridium chapter 11'ed the market for lightweight sats in LEO has almost completely evaporated.
Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
might be a Ukrainian-built An-225 "Mriya". It has a larger payload capacity and might be more suited for the purpose, having been used to transport the Russian shuttle in the past.
Here is one of the photos.
Why use an airplane for this sort of job? Why not use a tethered helium balloon instead? Balloons have great lifting capabilities, can go much higher than a conventional airplane, and would be much cheaper to operate. Have a balloon hoist the rocket up to 100K feet and shoot it out from there.
I seem to recall that DoD experimented with a similar idea in the '60s. A Polaris-like missile was pulled from the back of a cargo aircraft (C-130 or C-141) and, once hanging suspended, fired. The idea was dropped for several reasons, one of which was that it was not possible the accurately position the missile (vagaries of wind, chutes, etc.) accurately enough for accurate targeting. Perhaps modern computers can compensate for this.
"Love is a familiar; Love is a devil: there is no evil angel but Love." --William Shakespeare ('Love's Labors Lost')
Can't remember if the energy saved from the gain in altitude was enough to offset the other problems.