Posted on 08/12/2006 5:27:28 AM PDT by Paul Ross
H'mmm. Is this particular specification wise? Just because the Russians got away with it with Soyuz...i.e., here is Michael Cabbage's (Space Writer, Orlando Sentinal) posting relating to this:
NASA is designing the Ares 1 to lift off in much more marginal weather than the space shuttle. The goal is to create a vehicle more like Russias Soyuz booster, which has been launched in rain, high winds, fog and snowstorms.The first test flight of the rocket, dubbed Ares I-1, is scheduled for April 2009. The test will use an adapted four-segment booster from the shuttle program instead of the slightly longer five-segment version planned for operational flights. The second stage will consist of a dummy payload.
I never have liked solid-fueled rocket boosters for manned space flight.
Even if they were 100% reliable once they are lit you cant shut them down.
If something totally unrelated to the booster themselves goes wrong you have to wait till they have completed their burn to jettison the booster.
I hope the only piece of engineering they take from the shuttle over what they had on Apollo is, uhhhhhhhhh Hmmmmmmmmm. I'll have to get back with you.
It should lead to a more predictable, more economic space program. Designing aircraft to fly in "all weather", did the same for airline service. Of course, "all weather" isn't all weather, but rather all reasonable weather. Just out of curiosity, you didn't go to High School in Missouri did you Paul?
Last week I read that the plans for the Saturn V have been lost (along with the raw videotape of the moon landing). Maybe someone here knows if that is true.
Who was it who said, "The more things change, the more things stay the same."?
So after the multi billion dollar shuttle, we are going back to the man in a can approach.
Which works ok and is cheaper.
Nope, Minnesota.
It probably wouldn't matter if there were an O-Ring burn through on Ares I, as the fuel tank on that one (for the upper stage in this case) will be up on top of the SRB, not next to it. A burn through could screw up the trajectory, but shouldn't cause an explosion on Ares I.
On Ares V, if I get this right, it will look like the Shuttle tank with two SRBs attached directly to it as on the current Shuttle stack, but the rest of the stack goes on top as well. There are also liquid fuel engines beneath the tank. Frankly it will look much more like Russia's Energia or France's Ariane 5 when it's all up.
Ares I and Ares V
Energia vertical stack configuration:
Or the French Ariane 5:
There is no external tank to be breached and detonated on a vertical stack approach.
And the O-rings were fixed after Challenger. And even now, just to be extra-safe for the shuttle, they launch only in warm days so the material is at its most effective to seal...
It is good to not be sensitive to weather conditions. It is wise to not push your capabilities unless you really need to.
I would hope they do not try "bad weather takeoff" for anything but emergency rescue missions
Dont know about the Saturn plans, but R. Hoblein(sp?) was on the Art Bell Show (yeah, I know) a few weeks ago talking about how there are 700 boxes of raw footage, etc missing from the archives of the 1st moon landing.
?????
Another moon landing in 2020? 14 years from now? Pretty pathetic.
GM should do the same. Take apart a '63 Chevy and find out how the thing lasted 40 years and apply that to todays hunks of plastic junk.
With the solid boosters currently on the Shuttle, they still have a little fuel left over at the end of their burn phase.
I think the main reason for this is that they want to make sure that thrust from both boosters ends within a small fraction of a second; otherwise, the induced yaw would destroy the vehicle.
But they can't make a solid booster burn so precisely that it exhausts its fuel within a small fraction of a second of a nominal period. So, they equip the booster with a pyrotechnically-actived vent at the top.
When the solid boost phase is complete, they blow the vents on the boosters simultaneously, and this cuts off thrust immediately even though there's a small bit fuel remaining (varying slightly among the boosters).
Maybe solid boosters can be designed to be capablie of this early in the burn, for emergency aborts.
Restarts are not feasible in any solid booster design I know of, but present-day designers don't see this as a problem, so long as they add a liquid-fuel booster which gives a part of the total thrust, and which burns beyond the duration of the solid boosters.
But if the crew capsule can separate or eject that should solve that problem.
H'mmm. Is this particular specification wise?
From someone who thinks the current manned space program is a tragic joke, I think it's very wise. Can you imagine a commercial service surviving with the same delays as the Shuttle?
The original engineers of the space program did most of their calculations on slide rules. I wonder if having laptops is going to speed the process up. One can only hope!
NO2
Yes it is. They should shutdown the Shuttle and ISS, and get to it.
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