Re: SpaceX launch and live chat
- From: Joe Strout <joe@xxxxxxxxxx>
- Date: Tue, 20 Mar 2007 18:48:27 -0600
In article <Xns98F9B371B205Cdamon161attbicom@xxxxxxxxxxxxxx>,
Damon Hill <damon1SIX1@xxxxxxxxxxxxxx> wrote:
Do you still think they'll recycle? Last I heard they were (if I
understood correctly) draining the propellant from the vehicle, and
the video feed just shut off.
Yes, an immediate recycle and launch attempt is now in the works.
We'll see what happens...
Thanks for the tip; I see the video feed is back. They seem to be
holding at T-16 minutes. As you said: exciting!
- Joe
.
Relevant Pages
- The Next Lunar Landing - BOTE with NOX/HTPB
... per kg propellant cost) propellant combination - as used in ... This rocket is capable of 235 sec Isp, ... So, we might consider an 8 stage vehicle, with recovery of the larger, ... About 3 million tons. ... (sci.space.history) - Re: Google Cindy Sheehan (was: Re: Peace Mom)
... Let's design a hypothetical SSTO vehicle. ... It holds about 1.6 million lb of propellant at lift off. ... Next, we'll need some engines. ... There's no landing gear. ... (misc.writing) - Re: Shuttle proves being superb manned spacecraft
... This can be ameliorated somewhat by adding insulation to the outside of the tank, but now we have the issue of chunks of insulation hitting the vehicle. ... The ice formation/foam shedding only happens because of the use of cryogenic fuels in the tank, and it is only a hazard because the orbiter TPS is fragile. ... Choice of propellant, internal versus external propellant tanks, etc. Had the orbiter been equipped with internal propellant tanks, the peak entry temperatures would have been lower and a more robust TPS could have been employed, negating the debris problem. ... (sci.space.shuttle) - Re: Shuttle proves being superb manned spacecraft
... This can be ameliorated somewhat by adding insulation to the outside of the tank, but now we have the issue of chunks of insulation hitting the vehicle. ... The ice formation/foam shedding only happens because of the use of cryogenic fuels in the tank, and it is only a hazard because the orbiter TPS is fragile. ... Choice of propellant, internal versus external propellant tanks, etc. Had the orbiter been equipped with internal propellant tanks, the peak entry temperatures would have been lower and a more robust TPS could have been employed, negating the debris problem. ... (sci.space.shuttle) |
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