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Why NASA Rejected Lockheed Martin's Jupiter For Commercial Resupply Services 2 (fool.com)

MarkWhittington writes: Recently, NASA rejected Lockheed Martin's bid for a contract for the Commercial Resupply Services 2 (CRS-2) program as being too expensive. CRS-2 is the follow-on to the current CRS program that has SpaceX and Orbital Systems sending supplies to the International Space Station. Motley Fool explained why the aerospace giant was left behind and denied a share of what might be $14 billion between 2018 and 2024. In essence, Lockheed Martin tried to get the space agency to pay for a spacecraft that would do far more than just take cargo to and from the International Space Station.

36 comments

  1. The summing up is rather incorrect. by queazocotal · · Score: 2

    '$10000/lb - in fact it costs a lot more'.
    This is misleading - the costs quoted are for an entire developed system and sending it to ISS where it will also dock and return cargo.

    This is the difference between someone delivering 10 tons of sand to a dock on the other side of the country, and bagging it nicely in their own truck, and delivering it to your desk.

    1. Re:The summing up is rather incorrect. by Anonymous Coward · · Score: 3, Funny

      You managed to make a car analogy out of this. Luckily, I was able to decipher your meaning by referring back to the original story. On Slashdot, that is hard to do. Almost as hard as driving a Cadillac through the eye of a needle, if you get my drift.

    2. Re:The summing up is rather incorrect. by Coren22 · · Score: 1

      Drifting a Cadillac? That sounds tough...

      --
      APK likes to ask for responses to the same things over and over. Maybe he just likes the responses?
    3. Re:The summing up is rather incorrect. by budgenator · · Score: 1

      Nope, the ass of those old Cadillac Eldorados house-boats breaks lose pretty easy.

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
  2. Pigs get fat... by helixcode123 · · Score: 1

    ... hogs get slaughtered.

    --

    In a band? Use WheresTheGig for free.

  3. dear congress... by Anonymous Coward · · Score: 0

    if you keep cutting nasa budgets, nasa cant buy into overpriced out-of-scope contracts proposed by your major contributors. sorry about that.

  4. Reminds Me of This "Parable" by Anonymous Coward · · Score: 4, Funny

    THE KING'S TOASTER

    Once upon a time, in a kingdom not far from here, a king summoned two of his advisors for a test. He showed them both a shiny metal box with two slots in the top, a control knob and a lever.
    "What do you think this is?"

    One advisor, an engineer, answered first. "It is a toaster," he said.

    The king asked, "How would you design an embedded computer for it?"

    The engineer replied, "Using a four-bit microcontroller, I would write a simple program that reads the darkness knob and quantizes its position to one of 16 shades of darkness, from snow white to coal black. The program would use that darkness level as the index to a 16-element table of initial timer values. Then it would turn on the heating elements and start the timer with the initial value selected from the table. At the end of the time delay, it would turn off the heat and pop up the toast. Come back next week, and I'll show you a working prototype."

    The second advisor, a computer scientist, immediately recognized the danger of such short-sighted thinking. He said, "Toasters don't just turn bread into toast, they are also used to warm frozen waffles. What you see before you is really a breakfast food cooker. As the subjects of your kingdom become more sophisticated, they will demand more capabilities. They will need a breakfast food cooker that can also cook sausage, fry bacon, and make scrambled eggs. A toaster that only makes toast will soon be obsolete. If we don't look to the future, we will have to completely redesign the toaster in just a few years.

    With this in mind, we can formulate a more intelligent solution to the problem. First, create a class of breakfast foods. Specialize this class into subclasses: grains, pork and poultry. The specialization process should be repeated with grains divided into toast, muffins, pancakes and waffles; pork divided into sausage, links and bacon; and poultry divided into scrambled eggs, hard-boiled eggs, poached eggs, fried eggs, and various omelet classes.

    The ham and cheese omelet class is worth special attention because it must inherit characteristics from the pork, dairy and poultry classes. Thus, we see that the problem cannot be properly solved without multiple inheritance. At run time, the program must create the proper object and send a message to the object that says, 'Cook yourself'. The semantics of this message depend, of course, on the kind of object, so they have a different meaning to a piece of toast than to scrambled eggs.

    Reviewing the process so far, we see that the analysis phase has revealed that the primary requirement is to cook any kind of breakfast food. In the design phase, we have discovered some derived requirements. Specifically, we need an object-oriented language with multiple inheritance. Of course, users don't want the eggs to get cold while the bacon is frying, so concurrent processing is required, too.

    We must not forget the user interface. The lever that lowers the food lacks versatility and the darkness knob is confusing. Users won't buy the product unless it has a user-friendly, graphical interface.

    When the breakfast cooker is plugged in, users should see a cowboy boot on the screen. Users click on it and the message 'Booting UNIX v. 8.3' appears on the screen. (UNIX 8.3 should be out by the time the product gets to the market.) Users can pull down a menu and click on the foods they want to cook.

    Having made the wise decision of specifying the software first in the design phase, all that remains is to pick an adequate hardware platform for the implementation phase. An Intel 80386 with 8MB of memory, a 30MB hard disk and a VGA monitor should be sufficient. If you select a multitasking, object oriented language that supports multiple inheritance and has a built-in GUI, writing the program will be a snap. (Imagine the difficulty we would have had if we had foolishly allowed a hardware-first design strategy to lock us into a four-bit microcontroller!)."

    The king had the computer scientist thrown in the moat, and they all lived happily ever after.

  5. Horrible Article by gman003 · · Score: 3, Insightful

    So half of it sounds like Lockheed Martin whining that they lost the contract, even though as the biggest aerospace company they should have won. The writer either changed his mind halfway through and decided they deserved the loss, or just copied the first half verbatim from Lockheed Martin's press release.

    The other half is based on ignoring the word "development". Sure, the marginal cost to send a pound of stuff to space is about $10K. The cost to design a system to do so is considerably greater, particularly when you're developing not one, but three systems, for redundancy.

    And then he caps it off with "maybe we should just build a space elevator?", like the only reason we haven't done so is because it would cost too much, and certainly not because of the immense engineering challenges.

    1. Re:Horrible Article by Virtucon · · Score: 4, Interesting

      It's funny how government contract awards go. Losers whine and if the RFP hasn't been properly documented, vetted and scored then bidders can and have overturned decisions. It can even wind up in court based on federal procurement laws. In some cases fraud or collusion is involved while in others despite having an open process, a selected bidder can have an easier path through the process. The latter being the collusion part. For example a department writes an RFP and it goes out to bid for a new computer system that must be natively compatible with IBM's iSeries. Let's count how many bidders there may be.

      This is how you get overly priced items built for the government. It drowns in paper and bureaucracy including the annual "spend the budget" fun of summer where government agencies spend unused money on anything and everything because they don't want to risk the upcoming fiscal year budget. Rather than waving or giving the budget back to the treasury they'll spend it on anything they can.

      In reading the TFA it sounds like Lockheed did indeed come up with an overpriced system that had features that NASA didn't want. In reasonable cases that'd be it but all of the government contractors, not just aerospace, know how to game the system to the determent of all US taxpayers. It'll be fun to see if this gets dragged out. Fortunately there's two years until the next contract period and if Lockheed ultimately wins, the current contract holders will probably get paid at an escalated rate to deliver resupply missions because it'll be in their contracts as well since it's outside the agreed upon contract duration.

      --
      Harrison's Postulate - "For every action there is an equal and opposite criticism"
    2. Re:Horrible Article by dwywit · · Score: 2

      a new computer system that must be natively compatible with IBM's iSeries.

      Funny you should mention that. Way back when we wanted to replace an ageing System/36, we wanted to preserve the significant investment in the application code. Only Wang and IBM were in the running - Wang's system ran the '36 code by re-compiling the source into their own binary code, and IBM obviously bid an AS400. The final prices were (in my mind) suspiciously close. One of those two bidders had a mole in the competition.

      --
      They sentenced me to twenty years of boredom
    3. Re:Horrible Article by Virtucon · · Score: 2

      yeah, you could always guarantee that on those kinds of RFPs somebody had too much information. At a private company, we had a bid out for a replacement for an NAS/6 mainframe so IBM came in and bid a 3083 at twice the price of what National Advanced Systems (Hitachi) came back with. When a board member heard about awarding it to NAS, he became upset since he was a former IBM guy. He convinced the board not to approve the funding and buy IBM. That 3083 was a big piece of shit but we had the foresight to have performance penalties in the contract so IBM basically gave it to us for free.

      --
      Harrison's Postulate - "For every action there is an equal and opposite criticism"
  6. Re: Who gives a fuck? by Anonymous Coward · · Score: 0

    I'm a lesbian albino midget, you insensitive clod.

  7. This article is just a poor, unsubtle advert by Anonymous Coward · · Score: 3, Insightful

    It's a crappy article. It says that Lockheed Martin should have "by all rights" won the contract, even though it then admits that their bid was the highest and was just a way to get NASA to fund their own private goal to build a space tug, which NASA doesn't want and can't afford. And then to bring up a space elevator as though it's a reasonable, inexpensive alternative? What in the hell?

    Of course, it caps off with this, and it's then obvious that they just spent a couple minutes summarizing articles from other sites so they could add in their own advertising to it:

    The next billion-dollar iSecret
    The world's biggest tech company forgot to show you something at its recent event, but a few Wall Street analysts and the Fool didn't miss a beat: There's a small company that's powering their brand-new gadgets and the coming revolution in technology. And we think its stock price has nearly unlimited room to run for early-in-the-know investors! To be one of them, just click here.

    Wow, it's just like a good 30% of the spam I regularly get.

  8. Mission Creep by EnsilZah · · Score: 4, Interesting

    I like the idea of a space tug that can refuel and move satellites in orbit, but this role seems to be at odds with bringing cargo to the ISS which is the goal of the CRS(2) contracts.

    From what I understand the plan goes like this: On the first flight Jupiter (the tug) and Exoliner (the cargo vessel) go up together, once they are in orbit Jupiter adjusts the orbit to reach the ISS, after the cargo is offloaded and garbage is loaded Jupiter puts Exoliner on a path to burn up in the atmosphere while it itself stays in orbit to pick up the next Exoliner that's launched alone, as well as other tug duties.

    So the problem as I see it is this:
    For a tug you'd probably want a much more efficient ion drive to avoid refueling often, fuel boiling off and the like, you probably want the robotic arm that grabs on to wayward satellites.

    For supply deliveries you probably want liquid engines because some of the supplies and experiments are perishable and can't afford to wait the weeks or months it would take an ion engine to boost them to ISS orbit.
    And the grabby arm is redundant mass because the ISS has its own arm that's quite proficient at berthing other vehicles like the Dragon or Cygnus.

    So it looks like a compromise of design that's intended to get NASA to pay with the cargo delivery contract for unrelated functionality.
     

    1. Re:Mission Creep by Anonymous Coward · · Score: 0

      That's not unusual. Consider the other possibility for a "tug": not servicing satellites, but capturing or disabling them without polluting the orbit. That's been the holy grail of space defense for many years, and some say that the Shuttle and X37b were designed with that in mind.

      NASA gets its cargo, and DOD maybe gets to pay an undisclosed share of the development cost, in exchange for a few unreported activities on orbit.

      Most NASA projects that weren't unmanned probes had some sort of dual functionality: the Hubble was a cousin of Keyhole, the Shuttle had military capabilities, and so forth. Since one budget is black, you don't really know what they cost, or whether DOD offloads the cost onto NASA or if NASA is doing missions cheaper because they're using DOD funding/tech.

    2. Re:Mission Creep by Megane · · Score: 2

      Except that it's really hard to change the direction of an orbit. As in lots of fuel hard. If you send it up to dock with ISS, it's on the ISS orbit. To change it to, say, a polar orbit would require it to cancel much of the eastward orbital velocity, while adding velocity toward a polar orbit, and all the time still moving at the same "horizontal" speed to stay on orbit. (Going up and down in the same orbit isn't a problem, though.) So you have to choose your orbit while you go up, or bring a lot of extra fuel, orbital mechanics is a bitch that way.

      And ISS is already in a pretty useless orbit for most other stuff, being so far off of the equator so that Russia can reach it more easily from Baikonur. So the "tug" will be useless for anything but "helping" less-capable capsules to dock, in a way that they shouldn't need help, because ISS already has an arm. Yeah, maybe their idea wasn't so great after all.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    3. Re:Mission Creep by ColdWetDog · · Score: 1

      Depends on how patient your are. A solar powered ion thruster and a couple of years can do it. That said, you probably wouldn't use the same tug for ISS related work and pulling down errant satellites. You would think carefully about which sats you wanted and work from there.

      --
      Faster! Faster! Faster would be better!
    4. Re:Mission Creep by Anonymous Coward · · Score: 0

      Na, just takes longer, with a large number of directional thrusts at apops and periaps to change the inclination to a polar orbit. But it is just much more efficient to launch in the right direction in the first place.

    5. Re:Mission Creep by Anonymous Coward · · Score: 0

      You're assuming that only one or two get built, and that it gets/they get parked by the ISS. I'm suggesting that several get built and put into various orbits popular with the spooky crowd, while only one or two are made public.

    6. Re:Mission Creep by Overzeetop · · Score: 1

      No. No it doesn't. An inclination change requires a basic amount of delta-V for a give orbital altitude. It's done at apoapsis for maximum delta theta for a given delta V. Making a change at periapsis will be the most expensive place to change.

      --
      Is it just my observation, or are there way too many stupid people in the world?
    7. Re:Mission Creep by Anonymous Coward · · Score: 0

      A solar powered ion thruster and a couple of years can do it.

      No it can't, at least not in our lifetime and with the amount of fuel the ion thruster can carry. There simply isn't enough energy there to change the orbit.

      This same science fiction keeps coming up. Just go out and grab an asteroid to get some water. Run out to the Kuiper Belt to capture some minerals. Put a thruster on the side of an asteroid to move it out of a collision course with Earth. It won't work.

    8. Re:Mission Creep by budgenator · · Score: 2

      I don't think so, most of your energy budget is spent just getting to any orbit. Changing inclination is trivial because it's a zero-work manoeuvre as momentum is conserved, one burn starts you changing inclination and it continues until you do a breaking burn. Changing altitude is expensive because you have to accelerate out of the gravity well.

          ISS is orbiting at 409 km - 416 km with an orbital inclination of 51.65 degrees and orbital period of 92.69 minutes, a Molniya orbit is inclined 63.4 degrees and orbital period of 720 minutes, tungra orbits are inclined 63.4 degrees and orbital period of 1,436 minutes and Clarke orbits have 0 inclination and an orbital period of 1,436 minutes

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
    9. Re:Mission Creep by david_thornley · · Score: 2

      Most of the energy is spent getting to orbital speed, not getting the necessary altitude. Changing the inclination of the orbit is expensive in energy.

      It's not just a quick burn and the orientation starts to change; that's more like spaceship altitude. You have to change the velocity (defined as speed with direction).

      Say you're in an equatorial orbit, so your velocity vector points along the equator. Now you want to get into a polar orbit, in which the velocity vector is at right angles to your original, and just big in magnitude. This means you have to change velocity by the difference between the two, which is about 40% greater than the energy needed to reach orbital speed. You'd be better off landing and launching again in a polar orbit. That way you can have your original speed vector reduced to zero by atmospheric braking.

      --
      "When you have eliminated the unacceptable, whatever is left, however improbable, must be the truthiness" - Holmes
    10. Re:Mission Creep by budgenator · · Score: 1

      Most of the energy is spent getting to orbital speed, not getting the necessary altitude.

      Changing the inclination of the orbit is expensive in energy.

      Orbital speed and altitude are functional, if you want to increase altitude, you just accelerate to a higher speed, changing speed takes work in orbit. On the moon you can orbit just inches above the highest obstacle in your path.

      The velocity of an object is the rate of change of its position with respect to a frame of reference, and is a function of time. Velocity

      In orbit you frame of reference is the center of gravity of the Earth
      to change inclination, Newton's First law applies

      When viewed in an inertial reference frame, an object either remains at rest or continues to move at a constant velocity, unless acted upon by an external force Newton's laws of motion

      you just give the satellite a quick burn at a vector giving it a lateral motion and it begins to move and doesn't stop until you do a breaking burn, I.E Newton's first Law, how much energy it takes depends on how quick you want to get there; the geographical location of abstract surface details like the equator or the rotational pole are meaningless to the satellite.

      Think about it, what is easier walking 130 feet across a parking lot or walking up 13 floors worth of stairs? If you roll a bowling ball across the parking lot it keeps going until friction consumes it's kinetic energy, try rolling it up a handicap-ramp and see how quick gravity eats up the kinetic energy!

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
    11. Re:Mission Creep by david_thornley · · Score: 1

      A rule of thumb for orbital mechanics: the spacecraft will return to where it was, in position and velocity, as of the last velocity change (unless it runs into something). (If there's other bodies exerting significant gravity, this isn't true, but it's close enough in LEO.)

      Therefore, without loss of generality, take a satellite in equatorial orbit at 5 miles/second and fire a burn to the south, delta-V 1 mile/second. This changes its velocity by adding a northward component to the eastward velocity. It is now in a stable orbit, same as if it had been launched. The orbit is not going to move without further acceleration, and it's nowhere near a polar orbit.

      You can represent velocity with vectors, and to change orbit 90 degrees you need to change the velocity vector 90 degrees. Draw a vector from the original velocity vector to the desired one, and that's the velocity that must be applied to change the orbit.

      --
      "When you have eliminated the unacceptable, whatever is left, however improbable, must be the truthiness" - Holmes
    12. Re:Mission Creep by budgenator · · Score: 1

      Therefore, without loss of generality, take a satellite in equatorial orbit at 5 miles/second and fire a burn to the south, delta-V 1 mile/second. This changes its velocity by adding a northward component to the eastward velocity. It is now in a stable orbit, same as if it had been launched. The orbit is not going to move without further acceleration, and it's nowhere near a polar orbit.

      What you are not getting is deltaV = acceleration; under Newtonian Physics things don't accelerate unless acted upon by a force. When something faster it is accelerating, when something goes slower it is still an acceleration.
      When you start your burn your velocity vector is 5mi/S.( 0 degrees),
        finish your burn your velocity is 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees
        15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.

      You could have just as easily pointed you engine at 45 degrees starboard and gone to 6.0828mi/s.9.4623 degrees and burned for the square root of 2 and increased your altitude at the same time.

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
    13. Re:Mission Creep by david_thornley · · Score: 1

      Delta-V is acceleration times time.

      Your calculations show that a delta-V of one-fifth of the original velocity moves the orbital inclination by 11.31 degrees, which isn't real impressive. If you want to make a 90-degree change, you need about 1.4 times the original velocity, which is better done by landing and getting sent up again on another rocket.

      --
      "When you have eliminated the unacceptable, whatever is left, however improbable, must be the truthiness" - Holmes
    14. Re:Mission Creep by budgenator · · Score: 1

      15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.
      then
      15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.
      then
      15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.
      which is 45 miles in 45 seconds
      then
      15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.
      then
      15 seconds later your velocity is still 5mi/S.0degrees + 1mi/S.90 degrees which = 5.099mi/S.11.31degrees, therefore you have 0 deltaV (delta = change), i.e. your velocity has not changed, but your moving to port at a steady 1 mi/s or 15 miles during that time period.
      The Earth's circumference is 24,901 mi so it would take about 1 hour, 45 minutes. that's not to shabby.

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
  9. Awww Lockheed Martin doesn't get overruns for once by RubberDogBone · · Score: 1

    Given how Lockheed Martin seems completely incapable of bringing in ANY project on time or budget it is fitting that they not be awarded any new contracts -yes I can dream anyway, especially with NASA where they simply don't have the option of asking for billions of extra dollars to cover bullshit overruns like the F-35 has seen.

    Nor can NASA afford to overspend on a project like the F-35 that cannot actually DO what it was designed to do.

    This company would be a criminal enterprise under normal circumstances in any other industry. But they get a pass for being so vital. And well connected.

    --
    Sig for hire.
  10. Re: Who gives a fuck? by davester666 · · Score: 2

    quick poll: bang or not?

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    Sleep your way to a whiter smile...date a dentist!
  11. The Motley Fool is a pump and dump house by Overzeetop · · Score: 2

    It used to be interesting counter-wall street advice way, way back. Now it's just click bait ads for pump and dump schemes to make them rich.

    Not that the ad and click-bait has anything to do with the article, but knowing who "wrote" meant that it was clear nothing of value or insight would be written on those pages.

    --
    Is it just my observation, or are there way too many stupid people in the world?
  12. Too expensive by Anonymous Coward · · Score: 0

    Space tug sounds good even in today space, in the future their uses will only expand.

    However if it is super expensive (like NASA says it is) then it uses become very limited to the most critical situations (which ISS resupply is not).

    Basically good tech, but probably will become really useful only after 2nd or 3rd iteration when they take costs under control.