lost 80 seconds of data...
... turns out to be:
L33t aL!3n h4X0Rs rUl3! N4sA uV3 b33n pWn3|)!!!!11111one111
NASA chiefs in charge of the agency's next-generation rocket program said on Thursday that their $445 million Ares I-X test flight was a success in proving the launch vehicle's design. After poring over preliminary data, project manager of Ares I-X test flight Bob Ess said during a conference call with reporters that the …
I mean, one rocket test every three years!? Not the NASA that put a man on the moon "before the end of the decade". Apollo 8, 9, 10 and 11 all happened in 8 months.
I'm complaining because at this rate I'll be dead before NASA get around to doing anything new and interesting. Come on, there's oceans of methane out there waiting to be the solution to the oil shortage. All we have to do is get up there and collect it! Pedal faster fool!
Hmm if NASA ever go into the space tourism business, remind me not to use them - I'm not sure I like their crteria of "success".
One would have assumed that the mission must must be accomplished according to the flight plan for the notion of "Success" to apply, not just "It didn't CATO therefore we succeeded".
Think I'll take my chances with the Ruskies.
It was bound to succeed. They took some well-tried components that individually worked and put them together (shuttle, saturn v) - to obviously it would work. Much like peanut butter works, jelly works, put them together and you get peanut butter jelly. It just works (with a baseball bat)
It was bound to succeed
Not entirely, although they certainly stacked the deck pretty heavily.
Dummy 2nd stage, dummy 5th segment is fairly timid and should not have been expected to cause too many problems. However the high length to diameter ratio (relative to recent vehicles) would be a concern. Changes of diameter going down the vehicle can cause trouble as you go through the sound barrier and the down played but pretty important changes to the grain (the shape of the hole cut through the solid propellant to profile its chamber pressure) are AFAIK still pretty difficult to model by CFD. Oh and the parachutes would have to be scaled up as I don't think the SRB casing could take the impact caused by the increased impact velocity generated by a 20% increase (1 segment) in the mass.
In what seems to modern NASA's SOP its a dummy 2nd stage on top of a shuttle SRB with a dummy 5 segment.
Except it's completely different.
Which well tried components from the Saturn V were you thinking of?