Is it still mandatory for "headless" Falcon 9 rockets to perform static fires? Or can they already have their payloads mounted beforehand?Personally, I think it has something to do with AMOS 6 as if it's forever burnt in SpaceX's memory.
The IXPE science team have been told that they have the same booster as Crew-1 which would make this B1061.5.
Static fire test complete – targeting Thursday, December 9 at 1:00 a.m. ET for Falcon 9’s launch of @NASA’s Imaging X-ray Polarimetry Explorer (IXPE) mission
IXPE is SpaceX’s fifth launch to-date for @NASA_LSP
This will also be the fifth flight for this Falcon 9’s first stage booster, which previously supported launch of Crew-1, Crew-2, SXM-8, and CRS-23
Updated NGA notice. December 5 is removed. December 6 is now the primary launch day with December 7 and 8 as backup days. No additional backup days were added.
Re: STP-3 launch December 6:Quote from: Ken the Bin on 12/05/2021 02:36 amUpdated NGA notice. December 5 is removed. December 6 is now the primary launch day with December 7 and 8 as backup days. No additional backup days were added.Scheduling "cutout" for IXPE on December 9?
Some images of the Falcon 9 fairing now sitting in the LC-39A pad hangar awaiting the return of the Falcon 9 after its static fire test.
Quote from: Conexion Espacial on 12/03/2021 08:52 pmSome images of the Falcon 9 fairing now sitting in the LC-39A pad hangar awaiting the return of the Falcon 9 after its static fire test.No encapsulation photos?
Quote from: kdhilliard on 12/05/2021 02:41 pmQuote from: Conexion Espacial on 12/03/2021 08:52 pmSome images of the Falcon 9 fairing now sitting in the LC-39A pad hangar awaiting the return of the Falcon 9 after its static fire test.No encapsulation photos?Few posts before: https://forum.nasaspaceflight.com/index.php?topic=48510.msg2317251#msg2317251
Quote from: soltasto on 12/05/2021 02:43 pmQuote from: kdhilliard on 12/05/2021 02:41 pmQuote from: Conexion Espacial on 12/03/2021 08:52 pmSome images of the Falcon 9 fairing now sitting in the LC-39A pad hangar awaiting the return of the Falcon 9 after its static fire test.No encapsulation photos?Few posts before: https://forum.nasaspaceflight.com/index.php?topic=48510.msg2317251#msg2317251Right. (That's the post I quoted.) But they just show the caged fairing, not IXPE.For that matter, I can't find any cleanroom photos with a nearby human for scale.All we have are the two photos in this post.We've had nothing to give a sense of its size.
Quote from: soltasto on 12/05/2021 02:43 pmQuote from: kdhilliard on 12/05/2021 02:41 pmQuote from: Conexion Espacial on 12/03/2021 08:52 pmSome images of the Falcon 9 fairing now sitting in the LC-39A pad hangar awaiting the return of the Falcon 9 after its static fire test.No encapsulation photos?Few posts before: https://forum.nasaspaceflight.com/index.php?topic=48510.msg2317251#msg2317251Right. (That's the post I quoted.) But they just show the caged fairing, not IXPE.For that matter, I can't find any cleanroom photos with a nearby human for scale.All we have are the two photos in this post.We've had nothing to give a sense of its size.Edit: I just hope they aren't holding back such photos in response to the confusion over Zurbuchen's misunderstood joke about not receiving a discount for all the unused space in Lucy's fairing.
If you go to the Ball Aerospace IXPE page there is a clean room photo with a standard human and also a video of the boom extension test.
I wonder why this mission is not RTLS? A lightweight payload to LEO...
Quote from: Comga on 07/08/2019 09:29 pmNSF member OneSpeed calculated that the "Block 5" Falcon 9 could put 1800 kg into an equatorial orbit by combining the circularization burn with the enormous plane change. This is many times the mass of IXPE.Here's a simple way to figure out the capacity of F9 to such an orbit. First, find circular velocity at 540 km, about 7600 m/s.Then find a 27.5 degree plane change (usually the first stages can get rid of about 1o of inclination). It's about 3612 m/s. The circularization part of this burn will add very little, since the direction is different.If applied straight ahead, this delta-V would be beyond escape, and correspond to a C3 of about 11.Now you can go the LSP performance calculator, and plug in C3=11, and see what payload you can get. (You actually need to use C3=10, that's as far as F9 goes, and then get plots and extrapolate. I guess they never planned for payloads this light.) This gives about 750 kg for RTLS and 2100 kg for ASDS recovery.
NSF member OneSpeed calculated that the "Block 5" Falcon 9 could put 1800 kg into an equatorial orbit by combining the circularization burn with the enormous plane change. This is many times the mass of IXPE.