SpaceX skipping Red Dragon for “vastly bigger ships” on Mars http://www.teslarati.com/spacex-skipping-red-dragon-vastly-bigger-ships-mars-confirms-musk/ …pic.twitter.com/fyJNU4gmpt
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How do you get a 9m vehicle from Hawthorne to Boca Chica or the Cape?
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It could just do a sub orbital hop.
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Just stick it on the roof of the Hawthorne factory and let 'er rip!
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Get a bigger diameter boring machine...
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THAT is a number we can sink our teeth into! But how would you move a 30 foot diameter vehicle to the launch sites? By road to a sea port?
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Elon would have to do some serious roadwork to get a 9 meter diameter rocket stage to the beach from
#SpaceX's factory in Hawthorne L.A. -
How do you feel John about spacex skipping red dragon, no crewed propulsive dragon landings?
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Red Dragon & propulsive Dragon 2 landings were both long shots anyways. Elon is right to focus on what's already on his plate, not dessert!
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Will this replace Falcon all together?
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Reddit speculation says quite likely. Already cheaper than a F9 launch, and fully reusable, not to mention the insanely low per kg cost.
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I think not having to fly the FH is the biggest perk
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Downsized ITS might replace FH, eventually, but it would be overkill for most LEO payloads… unless they do multiple-berthed LEO launches.
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1/2 Multiple launches will help to gain huge profits: they could charge full price for each customer and still be the cheapest option by far
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2/2 Also, being overkill only means longer reentry burns and less damage to the booster. It is super cheap anyways.
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Hard to qualify what overkill is in the new reusability paradigm. Completely new frontier, lots of unknowns
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Looks like we'll find out in a couple of years (hopefully ≤ 5) just how much pent up demand there is in the launch market.
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So a 25% narrower vehicle at first. I take it the first stage will probs have about 24 engines instead of 42 based on change in base area.
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21 engines would fit perfectly. Just remove the outer ring from the original design.
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@FFairing: Your descendants won't only be reusable, they'll stay with the vehicle, opening clam-shell style to deploy payloads then closing. -
I had thought about that. But wouldn't it be less practical since u'd have to haul the extra mass of the fairing all the way to orbit?
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Even a 25% reduced size ITS would have more than the margin necessary to carry the faring to orbit. Reusability is a more important priority
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True, with fairings currently costing upwards of 5M, and I only see that becoming a larger figure as they are scaled up.
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All of the upper stage/spacecraft of the reduced size ITS will look the same from the outside: satellite launcher, tanker, passenger/cargo…
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For the passenger/cargo version, I propose 50 passengers on top in an abort capable Dragon 3 with 50t of cargo in a compartment below it.
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