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ISP of compressed air - Larry Niven idea
(Jake McGuire) wrote in message . com...
Michael J Wise wrote in message ... If you compress air to near-degeneracy, will it react to form nitrogen oxides? And it STILL has an ISP of 1. It's not going anywhere. I can't claim to be able to calculate the Isp of this hypothetical rocket, but given that basically-equivalent cold-gas thrusters have specific impulses in the 70 second range, I'm fairly confident that it's not 1. Yes, a cold gas thruster can give an exhaust velocity of up to 2x the speed of sound in that gas. 70 seconds of Isp sounds about right. 70sec of Isp into 10km/s of deltaV gives a mass ratio of about 1.6 million to one. HOWEVER: Back in 2001, the NY Times reported on metasable nitrogen crystals: http://www.nytimes.com/2001/05/22/science/22NITR.html Nitrogen forms a solid at about 2 million atmospheres that is stable at normal atmospheric pressure as long as you keep it chilled below 75K. There is an impressive amount of stored energy in these nitrogen polymers, and a metastable nitrogen monopropellant would have an Isp greater than 400 sec. If a means for producing metastable nitrogen can be found that would cost less than about $20/kg, rocket designers would rush to build engines that would use it as a propellant. The hot nitrogen in the exhaust would not be completely pollution free, since it would form nitrogen oxides when it reacts with normal air. It just goes to show you, that sometimes you can be right by accident. |
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