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Next NASA Vehicles To Resemble Shuttles
ausoleil writes "Spaceref.com has an internal NASA memo outlining potential plans for the next generation of launch vehicles. They will closely resemble the current Shuttle and use some of the same hardware. Of course, they plan to leave the exploding parts out of their next versions. From the article: 'NASA has decided to build two new launch systems - both of which will draw upon existing Space Shuttle hardware. One vehicle will be a cargo-only heavy lifter, the other will be used to launch the Crew Exploration Vehicle.'"
This memo could be a photocopy of something circulating thirty years ago. Sounds like they're finally going to take advantage of the modular parts of the shuttle the way they talked about when the shuttle stack design was being originally being funded twenty-five to thirty years ago. One nice change is that the rumor mill believes the heavy lift stack bears a striking resemblance to Robert Zubrin's Ares stack (a.k.a. Shuttle-Z).
The "Shuttle-C" cargo stack (and variations) were originally publically discussed in the early '80s as reasons why the shuttle was worth all we were spending (you don't just get the shuttle, you also get a "normal" heavy-lift launcher). Those variants, however, have had problems that could only be resolved by massive cultural change at the NASA level. One of the biggest issues was payload capacity of the side-slung configuration. Since then variations including the Ares stack and the more recent Shuttle-B have appeared and pretty much gone nowhere.
I suspect that the United Space Alliance's (USA's) "risk averse" culture will actively hinder and ultimately frustrate all of these plans. If you've ever worked for a government contractor, you'll understand the culture I'm talking about. They (Boeing and Lockheed-Martin, the companies in the USA partnership) don't have to compete in markets, and are positively allergic to any hint that they may have to compete with other companies for revenue. If NASA's hoping for bargains, they won't find them when dealing with USA.
Regards,
Ross
So, as always, (good science/actual military need/sensible budget-keeping (pick appropriate phrase based on article) ) takes a backseat to Senator Whosit saying, "You won't cost my state jobs!"
Have you been touched by his noodly appendage?
Overall, not a bad idea--it will be a Saturn V class booster. I am not crazy about using 6 SSMEs however, they are designed to be reusable, not flown on an expendable booster and are expensive as hell (about $300 million for the 6 first stage engines alone) Also, I seems to only speak of using 2 SRBs in the in-line HLLV, it would seem to me to make more sense to use 4 or 6 clustered around the core. After all, the shuttle SRBs are some of the cheapest power you can get.
Take the case of SkyLab vs. the International Space Station. According to Wikipedia, the two stack up as follows:Now with some simple math, we find that SkyLab averaged 77,088 kg per launch which the ISS averages about 8,380 kg per launch.
If you didn't just do a double take, you should have. The booster that lifted SkyLab stuck over 9 times the mass into orbit that current ISS flights do! Just what is going on here?
The answer lies in the Saturn V Booster vs. the current Space Shuttle. A three stage Saturn V had a maximum payload of 118,000 kg. (That's enough to send the entire ISS up in only 4 flights.) The Space Shuttle, OTOH, only has a cargo of 28,800 kg to LEO. So why does NASA want to reuse the tech? Because of the weight of the shuttle itself.
The Space Shuttle orbiter weighs in at a whopping 104,000 kg! Combined with its cargo capacity, the Space Shuttle is capable of 132,800 kg to LEO! That's way more than the Saturn V could manage on all three stages. So if we ditch the orbiter itself, the shuttle's infrastructure could be the most powerful superbooster ever designed.
Javascript + Nintendo DSi = DSiCade
The solid boosters ignition starts with a small Nasa Standard Initiator (NSI) http://www.hstc.com/pdf/nsi.pdf.
That then ignites a small pellet of boron / potassium nitrate.
Which ignites a small rocket motor which is about 4 inches long.
Which ignites a medium sized rocket motor about three feet long.
Which fires a jet of flame for about a tenth of a second, all the way down the whole inside length of the solid boosters, which ignites the whole inside at the same time.
Well, I've been trying to submit a story to slashdot over the past few days about a "parallel path" to government-built shuttle-derived that NASA recently announced, but I haven't had any luck. I've already had four or five variations on it rejected. Anybody have ideas on what might be wrong with the following submission?
At a recent talk, Michael Griffin outlined NASA's plans for helping to generate a robust and competitive commercial market in orbital spaceflight. The speech and Q&A transcripts from the talk are available. In a move reminiscent of the US government kickstarting the early airline industry by purchasing airmail services, NASA plans on supplementing government-derived transport by purchasing cargo delivery services to the International Space Station from commercial providers, followed by crew transportation after the systems have proven themselves. Unlike traditional government contracts, sellers wouldn't see a profit before the services are delivered and the emphasis will be on actual performance instead of process and specifications. Aviation Week has some commentary on the announcement.
On the one hand, I'm glad. The Shuttle has proved to be a horrible waste of money, a boondoggle of 1970s technology dictated by political pork and military paranoia rather than being designed for an actual specific purpose, and I'm glad it's going to be replaced.
It's just a shame that the only way we can get people out into space seems to be with 1960s technology rather than 2000s. At least, under the current government-funded model.
You must think in Russian.
Please, have a little respect. The "exploding parts" comment in the headline was uncalled for and childish.