Somehow, this new appalling concept reminds me of the old Iowahawk redneck haiku:
ENIGMA
Rusty paradox
Half Camaro, half Trans-Am
Yet it will not run
Fortunately, they’re unlikely to get the money to build this lawn ornament.
Somehow, this new appalling concept reminds me of the old Iowahawk redneck haiku:
ENIGMA
Rusty paradox
Half Camaro, half Trans-Am
Yet it will not run
Fortunately, they’re unlikely to get the money to build this lawn ornament.
Comments are closed.
Ugh. The Ares zombie… I just won’t die.
Great points in that link… though it’s a certainty the 5 seg wouldn’t automatically meet certification, as it’s an entirely different beast from the 4 seg SER (hence the many pillions it would take to develop).
Hrmmm, I’m shocked, shocked I say, that the airstart issue is being raised by that post… surely, a rocket engine that requires sea level air pressure and complex, massive launchpad ignition systems can’t be difficult to start in flight in a vacuum? Heck, just weld the lauchpad to the tail end of the rocket and launch it too, so it’d be there to provide ignition whenever needed (this would also solve the altitude issue by keeping the rocket at ground level).
Now there’s an unbiased source.
Oh, well, if it’s in an ATK press release, it must be true.
Translation: Dear Congress, please, please, please don’t close the pork valves.
OINK OINK OINK
Source
For those who’ve not seen Bill Whittles latest, you must watch this:
http://www.youtube.com/watch?v=2h_d6YVA1Kg
You think that’s bad, the United Space Alliance wants to try to continue the Shuttle for a mere $1.5 billion a year.
Well, it’s hard to beat the Ares design. The first stage used the SRB’s (with an extra joint for some more O-rings) while its second stage, of all the components and technologies in the Shuttle’s external tank, only used the foam. As an engineering manager, how do you top that? Well, by adding an Arianne, complete with political hairballs and language barriers. What do you bet that buried somewhere in the proposal is a requirement for a couple of specially built Airbus A-380’s to fly the upper stage across the Atlantic?
(Not representing my employer)
Best comments about this latest brain-fart over at Clark’s site:
– Bestowing of the title “super-corndog” for the proposed stack
– Gary Hudson asking for some of what the designers are smoking
– Trent Waddington asking that Clark not delete Gaetano’s trollmeistering, in order to prove for all to see how stupid an idea the super-corndog actually is …
This thing could best serve humanity by being a top ten on Letterman … 🙂
Best haiku evah!
I’ll have some of that as well.
Puff puff pass…
I have no idea what to say to this. If anything it firmly cements the notion that the people at the top of the traditional aerospace companies are designing things not with engineering expertise but with powerpoint.
I assume that ATK is so desperate to keep its gravy train going they will resort to any manner of hijinx to avoid having to face reality.
“Can I take your order?”
“Yeah, I’d like a super-sized corndog with bacon and cheese please…”
Hey, they have been proposing the SRB’s for heavy spacelift since SDI.
From 1987 🙂
http://www.astronautix.com/lvs/baranmdd.htm
Barbarian MDD
[[[It would consist of 3 Shuttle SRM’s, attached around a ring of six Delta RS-27 first stage boosters, which in turn clustered around a single Delta first stage booster that was the last stage of the launch vehicle.]]]
Talk about a real Frankenrocket…
Why should they stop now?
You know that that US Big Space is getting desperate when large-scale cooperation with the French space industry is its preferred course of action!
Naive curiosity prompts me to ask:
How much are ATK’s “improved” five-segment boosters supposedly going to cost? How much do Shuttle SRBs cost?
If ATK wants to sell solid boosters for launching crews into orbit, then why haven’t they backed a configuration consisting of two ordinary four-segment SRBs and an appropriately sized liquid-fueled stage between them? (Similar to the Direct Launcher proposals, but without something based on the Shuttle fuel tank and/or SSME as the liquid-fueled component.) Too expensive? Inefficient flight profile? Something else?
Ariane V as a second stage for the Stick. The mind boggles.
Comment seen at NASA Spaceflight Forum:
Ares 1, chop off it’s head, stake though heart, burn it, drop it to bottom of ocean, douse in holy water, shot with silver bullet, it doesn’t matter.
It will not die.
I need a drink.