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34 minutes ago, sevenperforce said:

Is it stretched? It looks stretched.

Don't believe it is. Looking at the NSF livestream and it's mounted slightly higher. The lack of fins and tiles also makes it look longer.

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this is either a lunar starship prototype or a tanker prototype. in either case it kind of makes sense you would omit the sea level engines. since it doesn't need to land it doesn't make sense to take those engines. on the other hand i doubt that this will be the initial test article. unless it could also be a dummy starship for super heavy testing. if they wanted to test without the added cost and complexity of having an actual starship in tow. 

anyone get a shot under its skirt, to see what kind of equipment it has? erm.

Edited by Nuke
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13 minutes ago, Nuke said:

this is either a lunar starship prototype or a tanker prototype. in either case it kind of makes sense you would omit the sea level engines. since it doesn't need to land it doesn't make sense to take those engines. on the other hand i doubt that this will be the initial test article. unless it could also be a dummy starship for super heavy testing. if they wanted to test without the added cost and complexity of having an actual starship in tow. 

anyone get a shot under its skirt, to see what kind of equipment it has? erm.

One thought is that the nose might have prop tanks, and in LEO it could attempt transfer within the vehicle with ullage burns as proof of concept before attempting vehicle to vehicle transfers.

Might also result in checking off some LSS milestones ($$$).

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7 minutes ago, tater said:

One thought is that the nose might have prop tanks, and in LEO it could attempt transfer within the vehicle with ullage burns as proof of concept before attempting vehicle to vehicle transfers.

Might also result in checking off some LSS milestones ($$$).

That is one of the tests NASA explicitly said was tracking, tank-to-tank transfer in the same ship. Seems pretty likely S26 or 27 will be the one to test it

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5 minutes ago, Beccab said:

That is one of the tests NASA explicitly said was tracking, tank-to-tank transfer in the same ship. Seems pretty likely S26 or 27 will be the one to test it

So they throw that honking big thing up into space - move fuel from one part to another and then deorbit for the check in the box?

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Just now, JoeSchmuckatelli said:

So they throw that honking big thing up into space - move fuel from one part to another and then deorbit for the check in the box?

Something like that, yeah. The last part isn't required, they have intertank cameras and sensors to check that, but it would be a bonus for sure

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4 minutes ago, Beccab said:

Something like that, yeah. The last part isn't required, they have intertank cameras and sensors to check that, but it would be a bonus for sure

If they don't deorbit... I'd like for them to say that it is remaining up there as a fuel depot and they have the ability to test ship to ship with it... otherwise you have a LOT of steel that could survive reentry just floating around.  Seems the responsible thing to do - if they aren't using it and don't want Chinese levels of PR problems.

Either have a purpose or toss it.

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36 minutes ago, JoeSchmuckatelli said:

If they don't deorbit... I'd like for them to say that it is remaining up there as a fuel depot and they have the ability to test ship to ship with it... otherwise you have a LOT of steel that could survive reentry just floating around.  Seems the responsible thing to do - if they aren't using it and don't want Chinese levels of PR problems.

Either have a purpose or toss it.

Oh it's definitely coming down yeah, it'd be a procedure like with F9 S2 stages. Deorbit burn, then straight to Point Nemo. I meant that I'm not sure if they want to do the test on a recoverable ship or not, since we don't have direct confirmation yet of exactly *what* S26/27 will do

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42 minutes ago, JoeSchmuckatelli said:

So they throw that honking big thing up into space - move fuel from one part to another and then deorbit for the check in the box?

With an expended SH (the norm for some time I would imagine) they can send it to TLI with ~1.1km/s to spare.

S26, that is.

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1 minute ago, tater said:

With an expended SH (the norm for some time I would imagine) they can send it to TLI with ~1.1km/s to spare.

S26, that is.

You know... that is an interesting point.

I've been laser focused on them trying to do the propulsive landing testing and proving the big boys can do it (or be caught) that I've not even given a moments thought about them sending stuff deeper into space.

I'd guess from a $$ standpoint that if the client is ready for them to toss a rock at the moon for grins, and Booster performs as advertised (lift-wise)... nothing would hold them back from commissioning a Booster as a traditional expendable.  The being able to land/catch and reuse isn't really a client-focused thing (when client is conditioned to expect expendable pricing)... but it is a cost-benefit to the company to be able to save money and then out-compete the competition on price.

Will be interesting to see what the next few years brings!

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1 hour ago, Beccab said:

Oh it's definitely coming down yeah, it'd be a procedure like with F9 S2 stages. Deorbit burn, then straight to Point Nemo. I meant that I'm not sure if they want to do the test on a recoverable ship or not, since we don't have direct confirmation yet of exactly *what* S26/27 will do

Hmm, I feel like this is tricky.

I have the feeling they will want to do prop transfer tests in a reasonably high orbit. If something goes wrong and they lose power, they don't want the thing making an uncontrolled re-entry before they can send up another ship to fix it.

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54 minutes ago, JoeSchmuckatelli said:

If they don't deorbit... I'd like for them to say that it is remaining up there as a fuel depot and they have the ability to test ship to ship with it... otherwise you have a LOT of steel that could survive reentry just floating around.  Seems the responsible thing to do - if they aren't using it and don't want Chinese levels of PR problems.

Either have a purpose or toss it.

I don't think its ready as an propellant depot. I need to have have an inverted quick disconnect connector so other ships can dock, I suspect also an upper docking point would be smart so all forces is not on the QD but should be possible without, but it has to be set up for docking. I would also expect it to be foamed for better insulation. 

But why not also use it to deploy starlink 2, yes they need to get the dispenser working. Or simply test it on an ship who also try to reenter? is an contracted time restrain on the test, or is the propellant to be pumped to much to allow for reentry equipment? 
If you have ullage, moving liquid between two tanks just require that its an pressure difference. Yes you have to deal with cryogenic propellant who makes this harder like how the hotter target tank will generate more gas so you want to went this gas as ullage or pump it to to the source tank. I see pumping between to ships as harder because the connection and you need to balance ullage between the this including the torque because of fuel transfer. 

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2 hours ago, Nuke said:

this is either a lunar starship prototype or a tanker prototype. in either case it kind of makes sense you would omit the sea level engines. since it doesn't need to land it doesn't make sense to take those engines. on the other hand i doubt that this will be the initial test article. unless it could also be a dummy starship for super heavy testing. if they wanted to test without the added cost and complexity of having an actual starship in tow. 

anyone get a shot under its skirt, to see what kind of equipment it has? erm.

The sea level engines has other uses than landing, first it add extra trust after separation increasing TWR, second and more important if one of the three vacuum engines fail you get out of center trust, an surface engine can gimbal and fire up to compensate. 
Yes if you don't need the extra TWR and don't care of an engine fail equal mission fail you can drop them but they will be on lunar starship for safety reasons. 

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Both Superheavy and Starship individually could theoretically SSTO, we think, with the right tank and engine configurations. So could F9 stage 1.

But the exact payload depends very heavily on the dry mass which isn't precisely known outside SpaceX at this point in development. If superheavy masses 160t, then it's payload SSTO with all sea level engines could be somewhere 5-40t range.

No rocket can SSTO and be recovered though, which is what makes it kind of pointless.

It will almost always be cheaper to recover the 1st stage and expend a smaller 2nd stage, even for the same payload.

Then consider that by expending a 2nd stage you can either massively reduce the size of the first stage needed for the same payload, or loft much more mass at once, and the economics of SSTO are very poor indeed.

Edited by RCgothic
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I suppose SH as a reusable Neutron-style smallsat launcher (RTLS first stage, very light second stage) would be too out-there. Even if it would be funny.

When's SH supposed to stage-separate? How far could it push this in terms of altitude and velocity before it was required to land at a downrange site (maybe that floating oil rig that we haven't heard of for a while)?

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1 hour ago, Geonovast said:

We have a whole thread for that exact question.

 

*reads* Much as I actually want to talk about it in the correct thread... I will not be sticking my face in to that crossfire of dogma. Then they moved on to just comparing SS/SH with other approaches.:mellow: I'll be good.

Edited by AckSed
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