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Lockheed Martin unveils Space Shuttle replacement

Vegan Bob writes "Lockheed Martin released its proposal for the Crew Exploration Vehicle (CEV) in a recent Popular Mechanics article. NASA will choose this vehicle scematic or opt for the yet-released Northrop Grumman design in 2008. The CEV will replace the Space Shuttle program, and will eventually go to the moon (between 2015 and 2020)."

9 of 549 comments (clear)

  1. One or two questions related to these articles: by Skyshadow · · Score: 5, Insightful
    Wait, what?

    Why add an orbital rendezvous requirement to all missions? Why use a shape like this which, I presume, requires the use of failure-prone ceramic tiles for reentry protection instead of a tried-and-proven heat sheild when you're planning to use parachutes to land the thing anyhow? What's the advantage to using this thing over just a regular capsule if it's not necessarily reusable?

    How does it possibly make sense to use the same vehicle for LEO missions as for moon and Mars missions? What happened to the important ideas behind Mars Direct or Semi-Direct (aka, having a seperate hab module that you can leave for future missions and making your fuel on Mars instead of hauling it with)? Does this signal that NASA is planning for Mars as just a set of "footprints and flagpoles" missions? Why are they planning a fly-by of Mars at all when the most dangerous part of a well-planned mission would be the part in transit rather than the part on the planet?

    And perhaps most of all, why is it going to take us fifteen years to get back to the moon when we got there from scratch in less than ten the first time around? Heck, what's our goal in going back to the moon in the first place instead of concentrating on the much-more-promising Mars? Did we miss something the last time around?

    In short: Just what, exactly, is going on here?

    --
    Every year during my review, I just pray the words "slashdot.org" aren't mentioned.
    1. Re:One or two questions related to these articles: by macpeep · · Score: 5, Insightful

      The benefit of a lifting body (or winged vehicle) is that you have more cross-track navigation control. Also, the g-loads on people inside the craft are much lower that way, which is good when they are coming back from a two year trip to Mars in zero gravity (or very low gravity while on Mars). Even for a long trip to the moon, it will be very helpful.

      Orbital rendezvous is good for a number of things. It allows you to have modularity so you can assembler larger crafts, add special modules later on that you haven't even thought of now (as more advanced technology becomes available 10 years down the road), use it to dock with the International Space Station, use it to dock with possible rescue crafts, etc.

      This is a vehicle for carrying people. It's not the full set of technologies needed to get to and land on Mars.

      And it's taking 15 years because there's no Soviet Union that's making everyone piss in their pants in fear.

    2. Re:One or two questions related to these articles: by JhohannaVH · · Score: 5, Interesting

      RTFA man.... and all you other commenters. Not only does it use a thermal shield instead of tiles, there IS a backup Carbon-Carbon shield.

      Also, this is not the final design, this is the one that Lockheed submitted for consideration in the competition. Final one to be chosen in 2008 with manned flights by 2014.

      I think that it's 'taking us so long to go go the moon' because the moon is most assuredly dead. It seems that the focus of everything is looking for life, which is great. Either that, or long-term bases on Luna, which is also great. If it's the latter, well, damn skippy it should take more than 15 years!!!! We've never tried to exist on another solar body, let alone one without supportive water or atmosphere.

      So, in answer to your question, this design is a stop gap measure to longer-term and better technically advanced systems to further our goal of living, flourishing and colonizing space and other bodies.

      --
      Sorry man... the Internet pooped on me.
    3. Re:One or two questions related to these articles: by stlhawkeye · · Score: 5, Interesting
      And perhaps most of all, why is it going to take us fifteen years to get back to the moon when we got there from scratch in less than ten the first time around? Heck, what's our goal in going back to the moon in the first place instead of concentrating on the much-more-promising Mars? Did we miss something the last time around?

      We didn't go to the moon for science and exploration, we went there to give the Reds a big fat middle finger.

      Further, NASA was a part of the United States Air Force at the time, not a separate entity with its own (very limited ) budget.

      Third, the Apollo project cost over $25 billion. In modern dollars, that's aover $100 billion. And believe or not, government spending was more efficient back then. Environmental impact studies weren't necessary, the cost of doing business was lower, the bidding process was simpler and cheaper. NASA's entire budget for this year is under $17 billion.

      You can't just reproduce the Saturn V and fly it. The Saturn V was too big for the launch facilities and it had to be assembled with its own tower and hauled out to the launch site.

      The Apollo program was also cut short. We'd made our point: America can reach the moon, and the Soviets can't. Neener neener neener. The last three moon missions were cancelled due to budget cuts.

      So why will it takes 15 years to get back there? Because none of our current technology is appropriate for the task, the old technology is not only unavailable (there's no more Saturn V's left that could fly) but updating it to modern standards and safety requirements (not to mention refocusing the moon landing to a science mission more than thumbing our nose at the Eastern Bloc) would probably cost as much or more than just starting from scratch.

      What's going on: I have no idea, but I honestly don't think they'll even hit the moon in 15 years unless some thing major changes about how NASA or the government does business.

      --
      "I have never won a debate with an ignorant person." -Ali ibn Abi Talib
    4. Re:One or two questions related to these articles: by Darth+Yoshi · · Score: 5, Interesting
      That should be followed up by the Z-prize, which either colonizes the moon continuously for a minimum period of time, or the first manned commercial Mars landing.

      Jerry Pournelle is way ahead of you.


      "I can solve the space access problem with a few sentences.

      "Be it enacted by the Congress of the United States:

      "The Treasurer of the United States is directed to pay to the first American owned company (if corporate at least 60% of the shares must be held by American citizens) the following sums for the following accomplishments. No monies shall be paid until the goals specified are accomplished and certified by suitable experts from the National Science Foundation or the National Academy of Science:

      "1. The sum of $2 billion to be paid for construction of 3 operational spacecraft which have achieved low earth orbit, returned to earth, and flown to orbit again three times in a period of three weeks.

      "2. The sum of $5 billion to be paid for construction and maintenance of a space station which has been continuously in orbit with at least 5 Americans aboard for a period of not less than three years and one day. The crew need not be the same persons for the entire time, but at no time shall the station be unoccupied.

      "3. The sum of $12 billion to be paid for construction and maintenance of a Lunar base in which no fewer than 31 Americans have continuously resided for a period of not less than four years and one day.

      "4. The sum of $10 billion to be paid for construction and maintenance of a solar power satellite system which delivers at least 800 megaWatts of electric power to a receiving station or stations in the United States for a period of at least two years and one day.

      "5. The payments made shall be exempt from all US taxes.

      "That would do it. Not one cent to be paid until the goals are accomplished. Not a bit of risk, and if it can't be done for those sums, well, no harm done to the treasury.

      "Henry Vanderbilt points out that having a prize, say $1 billion, for the second firm to achieve point (1) above will get more into the competition, and produce better results. I agree.


      --
      // TODO: fix sig
    5. Re:One or two questions related to these articles: by Rei · · Score: 5, Informative

      If you read TFA, you have a wild imagination to see some of the things in there that you claimed were in there. But to answer your questions specifically:

      Why add an orbital rendezvous requirement to all missions?

      We don't use the Shuttle for all missions, and the Russians don't use Soyuz for all missions. If we don't need humans or a rendezvou, we use Delta and Atlas rockets. You build to the mission, and this is built to the mission.

      Why use a shape like this which, I presume, requires the use of failure-prone ceramic tiles for reentry protection

      It says no such thing. In fact, from a reentry standpoint, this craft looks like what the shuttle was *supposed* to be, but wasn't because of budget constraints. It uses a titanium frame - this allows it to run hot on reentry, which means that heat dissipation issues aren't as serious, and damage isn't as threatening. A side advantage is you'll get a far better payload ratio.

      With a titanium frame, you generally only need to protect your leading edges, and they're using RCC, which is the best material out there in the present-day for such extremes (and isn't tiles). It's expensive, but it's a one-time production run, barring damage.

      Titanium frames also fatigue a *lot* less. In short, you get a safer, much lower maintainence, and longer lifespan craft. The only downside is higher initial cost.

      instead of a tried-and-proven heat sheild

      RCC is a tried and true heat shield. If you mean "ablatives", don't delude yourself into thinking that they're cheap, either - this will be far cheaper than ablatives when amortized over a few flights. Ablatives are costly and tricky to apply properly (just like other spray-on things, such as foam insulation) - and are very difficult to use around moving parts.

      when you're planning to use parachutes to land the thing anyhow?

      Parachutes don't slow you from orbital velocity. You might have noticed, if you had read, that it has wings. Do you know why? It's not to meet Buck Rogers Stylistic Guidelines(tm) - wings let you skim the atmosphere longer on reentry, burning off your heat slower. Then, on this craft, a drogue chute will fire, followed by the main chute. It's the best of both worlds - the wings can be smaller and optimized for hypersonic flight only, while they still give you a gentler reentry profile.

      it's not necessarily reusable?

      What cave are you living in that you didn't learn that the CEV was to be a reusable vehicle? The *launch vehicle* isn't expendible - it will probably be a modified Atlas or Delta, which are very good launch systems. Sure, I'd love to see a fully reusable booster that doesn't cost a fortune (which, by all means, should be possible), but one thing at a time.

      Overall, this is a great looking craft, and it will benefit greatly from all of the research that went on from the Shuttle program (and there was a *lot* - cost-reduction and safety-enhancing research was a good portion of the Shuttle's budget). My only real question is that its hypersonic drag profile looks a bit odd. Namely, there's no visible pinch as the wings widen (drag at hypersonic velocities is largely proportional to the maximum cross sectional area, so you typically pinch the fuselage as the wings eat up more cross section). I guess I'd also like to know why they chose ethanol biprop propulsion over, say, kerosene or LOX/propane. Still, great basic design principles on this craft.

      --
      It's a Cyrillic alphabet. It's like all those keys you never push on a calculator.
  2. I can see it all now... by StuffJustHappens · · Score: 5, Funny

    I haven't RTFA (hey, this is Slashdot!), but based on my observations of the shuttle landings - ie: like a 'regular' passenger plane, I can see how this all pans out:

    1. Moonbase 1 is built with a modern, high-tech arrivals terminal for the new craft.

    2. First craft arrives and personnel enter the arrivals lounge.

    3. Crew awaits baggage only to discover it's been sent to Mars.

    --
    --What's this sig thing all about then? Should I have one?
  3. X-33!?!? VentureStar!?!? by jzarling · · Score: 5, Insightful

    What about the X-33 and the VentureStar? Couldn't we just restart that program? The design is already worked out and the protoype of the X-33 was well on it way to completion.

    --
    It is better to be the hammer than the anvil.
  4. Don't go to the moon, blow it up by Is0m0rph · · Score: 5, Funny

    Like Arnold Schwarzenegger was saying on Howard Stern a couple weeks ago. The moon is not good for anything. The tides are a nuisance, most crime is committed during a full moon, female cycles follow the moon, no need for moonlight when we have fire and electricity. He said if he can't get government backing to blow up the moon he would go up there using his own money and blow it up himself.