Is it really all that hard to move stuff from LEO out to, well, out there? I was always told that the most expensive 100km in the solar system are the ones from ground to orbit.
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Hybrids could be good for getting up to LEO, but once you're up there... orbital adjustments and landing on the Moon would require throttlable, restartable motors. Maybe we should concentrate on a satellite first. Set a target altitude of 300km or so, then if we mess up on the orbit a bit, there's a big margin for error (maybe we screw up and it perigee's at 150km... at least it stays above most of the atmosphere, and stays up there)
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OTRAG was a German project to make a cheap launch vehicle; their rockets would have been made up of $8,000 twin-tank modules made of 12" pipe, fueled by nitric acid and kerosene. Cluster and stage a whole pile of these modules, and you're going to space. 81 half-size modules would get a minimum payload to LEO. 625 of them in 4 or 5 stages would lift 5 tons. There was a plan for a 10,000 module cluster (and it was UGLY!)
One site lists that a "Delta Class" OTRAG would use "a bundle of 60 modules, including a 6-module third stage nestled in an 18-module second stage, nested, in turn, in a 36-module first stage shell." Parallel staged, I guess.
But what if we built something similar? Cluster a whole pile of hybrids, and DON'T have an airframe around it. The cluster IS the airframe. Modules -- in our case, combustion chambers & N2O tanks -- just fall off when they're spent.
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I tried designing a CubeSat once. That's a satellite 10cm x 10cm x 10cm (just shy of 4" cubed) , weighing no more than 1kg (2.2 lbs), launched as a hitchiker payload. I wanted it to carry a simple ham radio repeater. I came across one problem: electrical power. Even covering the machine in solar panels, only a few of them will be pointing at the sun at any given time. And not only do you need enough solar power to run the satellite's payloads, but you need even more power to charge batteries so it'll work, or at least sleep and stay alive, in the shade. The hypothetical TRFSat would need even more power; radio transciever, computer, camera. TRF-Lunar would need even MORE power, because it has to shout a long way... and it'll need enough batteries to sleep for more than two weeks.
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I voulenteer to set up a downlink station in Vancouver, BC, Canada (120 W, 49 N).
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How about a series of missions? LEO, Geosynch, Lunar orbiter, Lunar lander (now that's going to be hard, because we need controlled landing motors)... Lunar sample return...
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Somebody work out how much thrust we need. Will this be something we could launch at LDRS, or are we renting a pad at KSC?
For that matter, are there laws governing private ventures to orbit? Do you have to file flight plans with anybody?
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Someone at the ESA was stoned the day they decided that Beagle 2's "hey mission control, I'm in place and I'm okay" message should be a song by Blur (though in spite of that, I really wish Beagle 2 had managed to broadcast it). I propose we use something classical. Or classic rock (Peter Schilling - Major Tom? ELO - Don't Bring Me Down? ELO - Ticket To The Moon? Boston - The Launch [instrumental]?). Or a forumite reciting some cool space quote ("Circling the Earth in the orbital spaceship I marvelled at the beauty of our planet. People of the world! Let us safeguard and enhance this beauty - not destroy it!" -- Yuri Gagarin) Or we could forget the music and have the **** thing start sending telemetry. Whatever works. Just... not Blur.