Author Topic: SpaceX FH : USSF-52 (X-37B OTV-7) : KSC LC-39A : 28/29 December 2023 01:07 UTC  (Read 210204 times)

Offline DistantTemple

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This is test launch on FH, with we (as argued variously up thread) guess a very large fule load. It seams they may be able to test various operations, as discussed up thread.

One type of real rapid response launch, for a real need, could be a launch on an F9, but obviously with somewhat less fuel, and less capeability to change orbits, however as long as itdidn't include GTO or other higher orbits it would still be very capeable. I guess if an X37B was standing by ready pretty much encapsulated etc, SX could launch it in a few days - just by bumping a Starlink mission!

The other type would be as mentioned above, an FH mission, loitering on orbit with masses of fuel. This second would be more secret, as changing launch perameters (F9) at very short notice would not be secret.
« Last Edit: 11/11/2023 04:15 pm by DistantTemple »
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Offline lrk

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Deep passes would face a heat soak problem that probably can't be addressed by the existing radiator, so you either are committing to landing somewhat soon after a deep pass (skipping stone reentry), or stuck with light passes.
Not even heat soak.   Just operating for long periods without the radiators deployed will be an issue.    Also, the service module isn't going to ride along for any dip in the atmosphere. 
These are reasonable concerns, but only if you did deep dips without designing for it.  Presumably, if they did this intentionally, they could close the doors just before the pass, and open them afterwards, so the radiators are only offline for a short time.  And the service module would be designed for dips.   It's quite strongly attached, and presumably could have at least some heat shielding on the exposed side - just enough for the dips, not re-entry level shielding.

I very much doubt they will try this, but if they if they did they would design for it, and I suspect could use much deeper dips than those used by unprotected spacecraft.

Why would the service module be needed during terminal aerobraking passes?  My understanding is that its main purpose is propulsion, and minimal dV would be needed after that point anyway.  Earlier missions flew without a service module entirely. 

They could potentially deploy the radiators between passes.  Or if that isn't feasible, they could have added an auxiliary cooling system such as a flash evaporator or ammonia boiler, like was used on Shuttle to help with cooling when the payload bay was closed. 

Offline Asteroza

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What about a dual payload and X-37 dropped off at a lower altitude.

In that case, fairing has to be expanded. Comparing with Falcon 9, if available mass is higher, volume isn't if fairing is the same.
This hypothesis requires the payloads to be stacked.
No,  there is room for more

There is room alright. X-37B and its service module can be mounted at least another 1 meter higher up into the fairing compared to the time it flew on Falcon 9.

So something ESPA Grande tower shaped below the service module? Something like Sherpa LTC or SHEPRA LTE, a propulsive tug? That would fit with the unmodified X-37/service module narrative pretty easily. Same with NG's LDPE, which has flown on Falcon Heavy before as well.

Offline Jim

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A major point of a military space plane (with large maneuvering capability) is rapid response.
Not when it is placed on a Falcon Heavy.
Not sure of this logic.   If you want fast response, presumably you want an asset already in orbit with considerable maneuvering capability (and hence a huge fuel load).  So you'd launch it on a big rocket (which is not fast response) so it's on orbit when you need it.

I always thought (but of course cannot confirm) that this is how imaging satellites work.   They launch on a big (not rapid response) launcher so they can later get where they are needed, when they are needed.

No,they keep the same basic orbit.  There is no "considerable maneuvering capability"  i.e plane change in LEO

Online LouScheffer

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Not sure of this logic.   If you want fast response, presumably you want an asset already in orbit with considerable maneuvering capability (and hence a huge fuel load).  So you'd launch it on a big rocket (which is not fast response) so it's on orbit when you need it.

I always thought (but of course cannot confirm) that this is how imaging satellites work.   They launch on a big (not rapid response) launcher so they can later get where they are needed, when they are needed.

No,they keep the same basic orbit.  There is no "considerable maneuvering capability"  i.e plane change in LEO
I too have never heard of a plane change.  I have heard informal comments (obviously unconfirmed) that they could and did maneuver in-plane to change the time of overflights, and to allow quite low perigees for critical imaging, plus a  subsequent reboost.  All rumors, but seem plausible.  The use of timing to avoid satellite overflights is well known, and a low but unsustainable perigee could double or triple resolution.

Offline Jim

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I too have never heard of a plane change.  I have heard informal comments (obviously unconfirmed) that they could and did maneuver in-plane to change the time of overflights, and to allow quite low perigees for critical imaging, plus a  subsequent reboost.  All rumors, but seem plausible.  The use of timing to avoid satellite overflights is well known, and a low but unsustainable perigee could double or triple resolution.

Current ones are in a 4 day repeating ground track. 
Not since Gambit have low perigees been used.

Offline daveglo

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What about a dual payload and X-37 dropped off at a lower altitude.
Jim, I get the idea of the opportunity on FH to do a dual-payload launch, but help me understand how that would align with the "expanding the envelope" and "new orbital regimes" comments in the press release.

Thanks for the insights!

Online LouScheffer

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What about a dual payload and X-37 dropped off at a lower altitude.
Jim, I get the idea of the opportunity on FH to do a dual-payload launch, but help me understand how that would align with the "expanding the envelope" and "new orbital regimes" comments in the press release.

Thanks for the insights!
I don't think there is any contradiction between "new orbital regimes" and a secondary payload.   A fully fueled X-37 can be guessed at about 20 tonnes (5 tonnes bare + 3100 m/s maneuvering fuel).  FH can put this into any practical orbit (it's rated at 26 tonnes to GTO) and still have payload mass to spare.  And new orbital regimes could be quite a bit less drastic than GTO.

Offline GewoonLukas_

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NextSpaceflight (Updated November 14th)
Launch NET 8 December 2023
https://nextspaceflight.com/launches/details/110

Does this mean we can assume launch December 7th local time and December 8th UTC?
Lukas C. H. • Hobbyist Mission Patch Artist 🎨 • May the force be with you my friend, Ad Astra Per Aspera ✨️

Offline Alexphysics

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NextSpaceflight (Updated November 14th)
Launch NET 8 December 2023
https://nextspaceflight.com/launches/details/110

Does this mean we can assume launch December 7th local time and December 8th UTC?

Yep. Evening launch local time, will be on the 8th in UTC. It'll be more clear once the launch window is announced.

Offline SpaceCadet1983

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Here is a first look at the USSF-52 X-37B OTV-7 mission patch.

Offline rocketenthusiast

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Here is a first look at the USSF-52 X-37B OTV-7 mission patch.
do they have the wrong falcon heavy configuration on the patch? or is there some experimental landing or something?

Offline SpaceCadet1983

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I wouldn't read too much into the depiction of the Falcon Heavy rendering on the patch.

Offline Kaputnik

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Not sure of this logic.   If you want fast response, presumably you want an asset already in orbit with considerable maneuvering capability (and hence a huge fuel load).  So you'd launch it on a big rocket (which is not fast response) so it's on orbit when you need it.

I always thought (but of course cannot confirm) that this is how imaging satellites work.   They launch on a big (not rapid response) launcher so they can later get where they are needed, when they are needed.

No,they keep the same basic orbit.  There is no "considerable maneuvering capability"  i.e plane change in LEO
I too have never heard of a plane change.  I have heard informal comments (obviously unconfirmed) that they could and did maneuver in-plane to change the time of overflights, and to allow quite low perigees for critical imaging, plus a  subsequent reboost.  All rumors, but seem plausible.  The use of timing to avoid satellite overflights is well known, and a low but unsustainable perigee could double or triple resolution.

Probably fanciful, but could they be exploring aerodynamic plane changes?
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Offline GewoonLukas_

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NextSpaceflight (Updated November 25th)
Launch NET December 2023
https://nextspaceflight.com/launches/details/110
Lukas C. H. • Hobbyist Mission Patch Artist 🎨 • May the force be with you my friend, Ad Astra Per Aspera ✨️

Online zubenelgenubi

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NextSpaceflight (Updated November 25th)
Launch NET December 2023
https://nextspaceflight.com/launches/details/110

Also here; my bold:
Ben Cooper's Launch Photography Viewing Guide, updated November 24:
https://www.launchphotography.com/Launch_Viewing_Guide.html
Quote
The next SpaceX Falcon 9 rocket will launch a Starlink batch from pad 40 on  November 27 at 11:00 p.m. EST or later. Upcoming launches include more Starlink batches from pad 40. A Falcon Heavy will launch the seventh OTV X-37B spaceplane mission for the U.S. Space Force from pad 39A on December. The side boosters will land back at the Cape eight minutes after launch.

I wonder what happened.
« Last Edit: 11/25/2023 05:00 pm by zubenelgenubi »
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Offline Zed_Noir

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<snip>
I wonder what happened.
Guess the X-37B is getting some new hardware installed and maybe some old hardware removed.

Don't think the Falcon Heavy is the cause of the launch date becoming uncertain. SpaceX already launch 4 of them this year.

Online ZachS09

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<snip>
I wonder what happened.
Guess the X-37B is getting some new hardware installed and maybe some old hardware removed.

Don't think the Falcon Heavy is the cause of the launch date becoming uncertain. SpaceX already launch 4 of them this year.


In layman's terms, it's "payload readiness issues". The two previous USSF Falcon Heavy flights were delayed because of that.
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Online zubenelgenubi

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How late can USSF-52 slip before impingeing on the IM-1 launch campaign? Circa the week before Christmas?  🎄 Two/2.5 weeks to shift GSE/pad from Falcon Heavy to Falcon 9?
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Offline DanClemmensen

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How late can USSF-52 slip before impingeing on the IM-1 launch campaign? Circa the week before Christmas?  🎄 Two/2.5 weeks to shift GSE/pad from Falcon Heavy to Falcon 9?
Does IM-1 require LC-39A, or could it move to SLC-40? Apparently, SX-3 may launch from SLC-40 instead of LC-39A now that SLC-40 has its shiny new crew access arm. AX-3 appears to have a bit more scheduling flexibility than IM-1, but I have lost track of all the constraints fro each of these missions.

Does USSF-52 impose the "must have time to evaluate the prior launch" rule?

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