It's not my first rodeojt2hunt said:TexAgs91 said:
No one should be making launch date predictions until SpaceX has its customary tangle with the FAA first.
Debbie downer
Fight! Fight! Fight!
It's not my first rodeojt2hunt said:TexAgs91 said:
No one should be making launch date predictions until SpaceX has its customary tangle with the FAA first.
Debbie downer
TexAgs91 said:
Received an overpressure notice for tomorrow (21st)!!! Booster 10 static fire test???? I really don’t know what to think but we’ll find out tomorrow! Go SpaceX!🔥🔥🔥
— Mary (@BocaChicaGal) December 21, 2023
@NASASpaceflight pic.twitter.com/lHag0DNOOM
Here is an enhanced view of the Starlink Pez dispenser door testing.
— Zack Golden (@CSI_Starbase) December 21, 2023
🎥: @LabPadre
✂️: @DeffGeff pic.twitter.com/wUUymggdiM
Bregxit said:Kenneth_2003 said:TexAgs91 said:
I saw that a week or so ago... That's one NOISY spacecraft!!!
Compared to what? I don't know that we have ever had video and audio from inside a spacecraft from orbit to the ground.
lb3 said:I think we're talking different retros.Ag_of_08 said:
The had one that had an issue after it had jettisoned it's Orbital module, but I can't remember the mission number. I swear Scott Manley talked about it at one point.
If I remember correctly they changed the order of operations after that, and now jettison the orbital module after the retro burn and separation, so if something goes wrong they could potentially make an emergency return to the ISS if retro fire fails( in you ditch the OM, it loses some of its rcs ability, and has no docking port)
I thought we were discussing the one that is triggered by a whip or rod contacting the ground a meter or so before touchdown.
Slow motion view of six-engine static fire pic.twitter.com/0O3H0jb9oq
— SpaceX (@SpaceX) December 20, 2023
OnlyForNow said:
So is the rocket bolted down during the static fire or do the engines not get anywhere close to full thrust?
How does the rocket not move any during these static fire events?
Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Kenneth_2003 said:Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Can they static fire the vacuum raptors at the test pad? I know they can use specialized facilities to lower the ambient pressures but I've only ever seen them discussed for single engine test stands. Firing at sea level with a vacuum optimized nozzle can lead to some violent shock waves from flow separation that can destroy an combustion chamber and therefore the whole engine.
Meanwhile, at Starbase...😅
— Chris Bergin - NSF (@NASASpaceflight) December 22, 2023
Potential Booster 10 Static Fire test. https://t.co/crIhHogU9t
Kenneth_2003 said:Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Can they static fire the vacuum raptors at the test pad? I know they can use specialized facilities to lower the ambient pressures but I've only ever seen them discussed for single engine test stands. Firing at sea level with a vacuum optimized nozzle can lead to some violent shock waves from flow separation that can destroy an combustion chamber and therefore the whole engine.
bmks270 said:Kenneth_2003 said:Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Can they static fire the vacuum raptors at the test pad? I know they can use specialized facilities to lower the ambient pressures but I've only ever seen them discussed for single engine test stands. Firing at sea level with a vacuum optimized nozzle can lead to some violent shock waves from flow separation that can destroy an combustion chamber and therefore the whole engine.
Vacuum engines are typically test fired without the full expansion nozzle.
Kceovaisnt- said:bmks270 said:Kenneth_2003 said:Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Can they static fire the vacuum raptors at the test pad? I know they can use specialized facilities to lower the ambient pressures but I've only ever seen them discussed for single engine test stands. Firing at sea level with a vacuum optimized nozzle can lead to some violent shock waves from flow separation that can destroy an combustion chamber and therefore the whole engine.
Vacuum engines are typically test fired without the full expansion nozzle.
SpaceX fires their Raptor Vacs in McGregor using a stiffener structure when performing full duration test firings. Flow separation does not get past the throat so the chambers shouldn't be at risk. Plus I do not think the nozzles are removable. I can't remember if the engines are film cooled or propellant loop cooled. I want to say it's the latter and therefore not removable.
I don't think firing Raptor Vacs at sea level is a problem without reinforcement at the short durations they fire them for Ship static fires.
I'm staying at Margaritaville right now. Didn't see anything.PJYoung said:Meanwhile, at Starbase...😅
— Chris Bergin - NSF (@NASASpaceflight) December 22, 2023
Potential Booster 10 Static Fire test. https://t.co/crIhHogU9t
I don't think anything is happening today. Road still open.
Next closure is Wednesday 8a til 8p.
bmks270 said:Kceovaisnt- said:bmks270 said:Kenneth_2003 said:Maybe this has been discussed, but it's something I literally just thought about...Decay said:Starship with only 6 engines is probably fine to go full tilt.Kenneth_2003 said:
I don't know about Starship, but for the Booster the static fire is at (IIRC) 50% thrust. The hold down clamps are not strong enough to hold 33 Raptors at full thrust. Shoot I don't think the booster is strong enough if the clamps could hold it.
Recall on IFT2 they released the clamps 30 minutes before launch.
I don't think they'd even bother trying to engineer a system to hold down 100% booster thrust. They're not even going to 100% during normal launch if I'm not mistaken.
Can they static fire the vacuum raptors at the test pad? I know they can use specialized facilities to lower the ambient pressures but I've only ever seen them discussed for single engine test stands. Firing at sea level with a vacuum optimized nozzle can lead to some violent shock waves from flow separation that can destroy an combustion chamber and therefore the whole engine.
Vacuum engines are typically test fired without the full expansion nozzle.
SpaceX fires their Raptor Vacs in McGregor using a stiffener structure when performing full duration test firings. Flow separation does not get past the throat so the chambers shouldn't be at risk. Plus I do not think the nozzles are removable. I can't remember if the engines are film cooled or propellant loop cooled. I want to say it's the latter and therefore not removable.
I don't think firing Raptor Vacs at sea level is a problem without reinforcement at the short durations they fire them for Ship static fires.
Thanks for the insight.
I found a picture of a vacuum engine test, and it looks like it's designed so that there isn't much flow separation at sea level.
Views of B1058 on the deck of Just Read the Instructions. Starlink 6-32 was the 19th launch and landing of this booster. The crew encountered rough conditions not far from Port Canaveral. Farewell old friend. @NASASpaceflight SCL views:https://t.co/lIR57w4WqB pic.twitter.com/6rew5JDySI
— Julia Bergeron (@julia_bergeron) December 26, 2023
Fair winds and following seas.
— Max Evans (@_mgde_) December 26, 2023
Following rough conditions in the Atlantic after the Starlink 6-32 mission, Falcon 9 first stage B1058.20 became unstable and tipped over on drone ship, Just Read The Instructions.
📸 - @NASASpaceflight
📺 - https://t.co/AFdPuCYKLR pic.twitter.com/clEGaxpeeR
#NASAWebb has had a busy year, and what better way to celebrate the telescope’s two years in space than to remember the science headlines it made in 2023! Credit: STScI. pic.twitter.com/Haf3A1zyjI
— Space Telescope Science Institute (@SpaceTelescope) December 25, 2023
Quote:
During transport back to Port early this morning, the booster tipped over on the droneship due to high winds and waves. Newer Falcon boosters have upgraded landing legs with the capability to self-level and mitigate this type of issue
Kansas Kid said:
I remember when a successful landing of these boosters was news. Now, they have made it so launches and recoveries so routine the only time you hear anything is if something goes wrong which isn't very often.
Long March 3B booster fell in Guangxi https://t.co/5L9yha3Liz pic.twitter.com/zb3Czc1Zgw
— China 'N Asia Spaceflight 🚀𝕏 🛰️ (@CNSpaceflight) December 26, 2023
Italian photographer Valerio Minato just won NASA’s Astronomy Picture of the Day pic.twitter.com/fWpziONEBj
— James Lucas (@JamesLucasIT) December 25, 2023
WAIT... was that the whole stage that failed to make orbit or a spent piece?PJYoung said:Long March 3B booster fell in Guangxi https://t.co/5L9yha3Liz pic.twitter.com/zb3Czc1Zgw
— China 'N Asia Spaceflight 🚀𝕏 🛰️ (@CNSpaceflight) December 26, 2023
Oh China.