When (first) orbital flight?First integrated flight test occurred April 20, 2023. "The vehicle cleared the pad and beach as Starship climbed to an apogee of ~39 km over the Gulf of Mexico – the highest of any Starship to-date. The vehicle experienced multiple engines out during the flight test, lost altitude, and began to tumble. The flight termination system was commanded on both the booster and ship."
What's happening next? SpaceX has assessed damage to Stage 0 and is implementing fixes and changes including a water deluge/pad protection/"shower head" system. No major repairs to key structures appear to be necessary.
Why no flame diverter/flame trench below the OLM?Musk tweeted on April 21: "3 months ago, we started building a massive water-cooled, steel plate to go under the launch mount. Wasn’t ready in time & we wrongly thought, based on static fire data, that Fondag would make it through 1 launch." Regarding a trench, note that the Starship on the OLM sits 2.5x higher off the ground than the Saturn V sat above the base of its flame trench, and the OLM has 6 exits vs. 2 on the Saturn V trench.
I'll attempt to keep this post current with links and major updates, but would be greatly helped by information supplied by the community. I hope this can be an alternate place to discuss Starship development. While the Starship Development Threads on Reddit are not party threads, Lemmy is still small enough that I don't imagine that strict moderation will be needed in the short term.
This is the finest FAQ in the fediverse. I come back to it, just to appreciate just how much data you fit in it, so easily accessible and concise for the experienced and inexperienced alike. It makes up for so many poorly written, ugly, inhuman FAQs across the years.
Unrolled tweet thread at threadreaderapp.com by Ryan Hansen Space @RyanHansenSpace. It's a look at the details of the steel plate parts and assembly under the Orbital Launch Mount.
I’m really impressed by how quickly the plate is getting assembled. I didn’t expect the manifolds to get added for another week or so, and now they’re at 2 / 3.
I’m not sure what the bottleneck is at the moment. Once everything is lifted in place they can move B9 over, but they might want to wait until they hit stage adapter is added.
B9 could go through spin prime tests without the plane being ready, and the plate can get tested without all deluge water & gas tanks present. We’re also it sure how far along the other OLM repairs are (cryo pipes are still being replaced). So there’s a ton of stuff happening in parallel.
9:15am cdt- 11 more loads of rebar have been lifted over to the OLM since midnight. LR11000 still holding the deluge pipe in position to be welded.
Edit-
10:48am- Deluge pipe is moved to the side of the underground pipe bunker and laid down on the ground.
11:50am- 8 more bundles of rebar have been lifted over to the OLM. Some presumably extra bent pieces have been lifted away as well.
1:11pm- Deluge pipe raised again and moved back to join the pipe that goes underground.
5:00pm- Since noon there has been 15 more loads of rebar craned over to the OLM. Most loads appear to be multiple pieces but there are several large bent pieces that have been moved one at a time.
9:00pm- 10 more loads of rebar have been moved over. (44 for the day so far and 56 in the last 40 hours)
I was summoned out of my Christmas lair for an update. I see the cladding was already mentioned.
Starbase live-
Yellow crane to the left of OLM has been lifting rebar over to the pit most of the day.
(I missed part of the morning but I’ve counted at least 12 loads so far)
Rover 2-
20:43 cdt- The large deluge pipe that we saw test fitted last night has now been painted white and is lifted back over to where the pipes go underground by the tanks.
Ship 25 completed a flight-like chill and spin of the Raptor engine pumps, stopping just before engine ignition. As a result of the test, cryogenic liquid oxygen formed a visible cloud beneath the ship. This checked out vital systems in advance of the upcoming static fire.
Looks like the segments are around 400mm thick and constructed from 40mm (38mm=1.5"?) steel plate The overall shape is a hexagon about 10m across the flats with each corner notched out.
They also speculated on how to weld the edges together: maybe put them on a stand above the final location, weld them from above and below, attach cranes and remove the stand, lower into place.
In a Twitter Space with @ashleevance, @elonmusk shares that Starship will hot-stage during the next flight, lighting engines on the ship with some engines still running on the booster, as to Never Stop Thrusting!™️
"Hot staging" is firing the upper stage engines while it's still nominally attached to the lower stage (like resting on or loosely attached). The advantages that I gather exist: It's fast. It takes care of stage separation without needing springs or little rockets or a flip or anything. Before firing a liquid-fueled stage that may have gases in a tank ("ullage"), you have to settle the contents so that the engine intakes suck only liquid (maybe using "ullage rockets"), but if you're still accelerating at separation, that's automatically taken care of.
But if you intend to reuse the first stage, well, I wonder whether six engines igniting will be too hard on it.
Apparently U.S. Titan rockets, a lot of Soviet / Russian ones (Soyuz, Progress, N-1), and (some?) Chinese Long March rockets were designed with hot staging.
Joe Barnard @joebarnard replies: "'okay so when I hot stage it’s “an anomaly” and I’ve “torched another flight computer” but when SpaceX does it it’s fine???'
"We made sort of a late-breaking change that’s really quite significant to the way that stage separation works," Musk said, describing the switch to hot staging. "There’s a meaningful payload-to-orbit advantage with hot-staging that is conservatively about a 10% increase."...
Musk said that, for Starship, most of the 33 Raptor engines on the Super Heavy booster would be turned off, but a few still firing, when the engines on the Starship upper stage are ignited. Doing so, he said, avoids the loss of thrust during traditional stage separation, where the lower stage shuts down first.
Doing so requires some modifications to the Super Heavy booster. Musk said SpaceX is working on an extension to the top of the booster “that is almost all vents” to allow the exhaust from the upper stage to escape while still attached to the booster. SpaceX will also add shielding to the top of the booster to protect it from the exhaust.
“This is the most risky thing, I think, for the next flight,” he said of the new stage separation technique.
Besides the change in stage separation, Musk said SpaceX made a “tremendous number” of other changes to the vehicle, “well over a thousand.” He didn’t go into details about the changes, ...
SpaceX also made improvements to the Raptor engines, with Musk describing the vehicle launching in April as using a “hodgepodge” of engines built over time. The Raptors on the new vehicles include changes to the hot gas manifold in the engine to reduce fuel leakage.
Those changes, he said, gave him more confidence in the success of the next launch. “I think the probability this next flight working, getting to orbit, is much higher than the last one. Maybe it’s like 60%.” In an online conversation in late April, he estimated a “better than 50% chance” of success on the next launch.
In another note, Musk finally learned some caution!
Musk, asked about any plans for a Starlink IPO, declined to comment. “It would not be legal for me to speculate about a Starlink IPO,” he claimed. “I think it’s against regulations to talk with any kinds of specifics about a future public offering.”
Edit: Peter Hague PhD @peterrhague: Thus far Musk estimates $2-3bn invested by SpaceX so far in Starship. The price of a single SLS launch
At stage separation how horizontal is Starship? If there was no vertical moment then how significant would the gravity loss actually be?
AFAIK most of the gravity loss is in the first few second of a launch but I don't have any idea what you are losing by the time you get to stage separation.
Interesting, most of the Soviet rockets that uses hot staging had a truss between each stage to allow the exhaust to vent. As far as I know starship doesn't have anything like this yet, I wonder if they'll add some or if they're just gonna see what happens without it 😂
Such a device has been spotted at the shipyard. It has been speculated that the reason the ship QD was removed was to adjust it for the height added by the vented spacer.
This is great thank you, I started following spacex Reddit in the echologic (was that his name?) Days, but the sub got a bit, I dunno, it started to lack a certain something. Just got too big maybe.
I'm happy to see this here! Thanks for starting it, sorry for the off topic 😂
More pour info, this time from tweets from Zack Golden @CSI_Starbase. The truck counts basically match those from @LettuceTurnipTheBeet@lemm.ee's post earlier.
SpaceX has received their final load of concrete for today's Orbital Launch Mount foundation work. Here are the totals after the 15.3 hour marathon:
June 25th - 132 Truck loads
July 3rd - 171 Truck loads
Total Volume = 2,302 m^3 = 3030 yd^3
Total Weight = 5,411 Tons
For reference, a Fully loaded Starship ~ 5,000 Tons
Note: There were 4 additional trucks that showed up but were turned back around without offloading.
Shoutout to agents @VickiCocks15 and @SpmtTracker for keeping track of all these.
4:11 PM · Jul 3, 2023
and
Obviously this number is significantly greater than we predicted. For those who asked, that previous number was not considering the area in yellow, which were also completed today. This area is technically outside of the true foundation of the OLM
RGV Sneak Peek shows some nice shots of the steel plates, as well as the pour under the OLM. Looks like a lot more concrete is needed though, wonder when that’ll happen.
The steel plates look ready for transport, so I bet this next pour will be soon — it seems to be the main hold up.
So the big news of the day and night was what is believed to be the center plate of the water deluge system. It is thought that it will be placed directly under the Orbital Launch Mount.
@LettuceTurnipTheBeet@lemm.ee already posted (at top level) "CSI Starbase video on new Deluge system", a deep dive part 1. The URL I see for the post is https://lemmy.world/post/879748 , because that's how I access this. The canonical one is https://lemm.ee/post/530280 .
CSI Starbase SPMT Tracker @SpmtTracker posted a tweet with a picture of what is very likely to be a vertical stand for the center plate. The image is on Imgur.The tweet is here. Ryan Hansen Space @RyanHansenSpace tweeted a rendering of how it might look under the OLM. This should be the image:
@LettuceTurnipTheBeet@lemm.ee posted below (if sorted by new) a link to a 13-minute video by Starship Gazer, of people working in the tent on the center plate. https://lemm.ee/comment/534238 . Someone commented that, from 4 minutes on, it's comedy gold. People were grinning around them. I'm told that someone is standing on top of the cheater pipe at one point.
NASASpaceflight posted a video of the rollout of the center. It's about 1 hour 26 minutes long. The stand / jig was on the first truck; the center plate with some people on it was on the next truck. The clearest views are about 17 minutes on.
Same to you, bud! I figure I'll keep blowing on the embers. Either the flame will catch (& I get to boast "I was into Lemmy before it really took off"), or my lungs will get too tired.
I know Twitter links are kind of impossible to follow right now, but don’t think I can embed an image in a comment. Anyway, that plate is huge, will be interesting to see them lift and transport it.
[Meta] Twitter is now throwing up a nag screen to force users to log in to view content, supposedly on a temporary basis. Since a lot of the content here links to Twitter, this could be inconvenient to those without an account.
A simple solution is to link to the embedded version of the Tweet, like so. Simply type:
SN15 and S20 are in the Rocket Garden, the rest are scrapped.
S24
In pieces in the ocean
Destroyed
April 20th: Destroyed when booster MECO and ship stage separation from booster failed three minutes and 59 seconds after successful launch, so FTS was activated. This was the second launch attempt.
S25
Launch Site
Testing
On Feb 23rd moved back to build site, then on the 25th taken to the Massey's test site. March 21st: Cryo test. May 5th: Another cryo test. May 18th: Moved to the Launch Site and in the afternoon lifted onto Suborbital Test Stand B.
S26
Rocket Garden
Resting
No fins or heat shield, plus other changes. March 25th: Lifted onto the new higher stand in Rocket Garden. March 28th: First RVac installed (number 205). March 29th: RVac number 212 taken over to S26 and later in the day the third RVac (number 202) was taken over to S26 for installation. March 31st: First Raptor Center installed (note that S26 is the first Ship with electric Thrust Vector Control). April 1st: Two more Raptor Centers moved over to S26.
S27
Rocket Garden
Completed but no Raptors yet
Like S26, no fins or heat shield. April 24th: Moved to the Rocket Garden.
S28
High Bay 1
Under construction
February 7th Assorted parts spotted. March 24th: Mid LOX barrel taken into High Bay 1. March 28th: Existing stack placed onto Mid LOX barrel. March 31st: Almost completed stack lifted off turntable. April 5th: Aft/Thrust section taken into High Bay 1. April 6th: the already stacked main body of the ship has been placed onto the thrust section, giving a fully stacked ship. April 25th: Lifted off the welding turntable, then the 'squid' detached - it was then connected up to a new type of lifting attachment which connects to the two lifting points below the forward flaps that are used by the chopsticks. May 25th: Installation of the first Aft Flap (interesting note: the Aft Flaps for S28 are from the scrapped S22).
S29
High Bay 1
Under construction
April 28th: Nosecone and Payload Bay taken inside High Bay 1 (interesting note: the Forward Flaps are from the scrapped S22). May 1st: nosecone stacked onto payload bay (note that S29 is being stacked on the new welding turntable to the left of center inside High Bay 1, this means that LabPadre's Sentinel Cam can't see it and so NSF's cam looking at the build site is the only one with a view when it's on the turntable). May 4th: Sleeved Forward Dome moved into High Bay 1 and placed on the welding turntable. May 5th: Nosecone+Payload Bay stack placed onto Sleeved Forward Dome and welded. May 10th: Nosecone stack hooked up to new lifting rig instead of the 'Squid' (the new rig attaches to the Chopstick's lifting points and the leeward Squid hooks). May 11th: Sleeved Common Dome moved into High Bay 1. May 16th: Nosecone stack placed onto Sleeved Common Dome and welded. May 18th: Mid LOX section moved inside High Bay 1. May 19th: Current stack placed onto Mid LOX section for welding. June 2nd: Aft/Thrust section moved into High Bay 1. June 6th: The already stacked main body of the ship has been placed onto the thrust section, giving a fully stacked ship.
S30+
Build Site
Parts under construction
Assorted parts spotted through S34.
Booster
Location
Status
Comment
Pre-B7 & B8
Scrapped or Retired
B4 is in the Rocket Garden, the rest are scrapped.
B7
In pieces in the ocean
Destroyed
April 20th: Destroyed when MECO and stage separation of ship from booster failed three minutes and 59 seconds after successful launch, so FTS was activated. This was the second launch attempt.
B9
High Bay 2
Raptor Install
Cryo testing (methane and oxygen) on Dec. 21 and Dec. 29. Rollback on Jan. 10. On March 7th Raptors started to be taken into High Bay 2 for B9.
B10
Rocket Garden
Resting
20-ring LOX tank inside High Bay 2 and Methane tank (with grid fins installed) in the ring yard. March 18th: Methane tank moved from the ring yard and into High Bay 2 for final stacking onto the LOX tank. March 22nd: Methane tank stacked onto LOX tank, resulting in a fully stacked booster. May 27th: Moved to the Rocket Garden. Note: even though it appears to be complete it currently has no Raptors.
B11
High Bay 2
Under construction
March 24th: 'A3' barrel had the current 8-ring LOX tank stacked onto it. March 30th: 'A4' 4-ring LOX tank barrel taken inside High Bay 2 and stacked. April 2nd: 'A5' 4-ring barrel taken inside High Bay 2. April 4th: First methane tank 3-ring barrel parked outside High Bay 2 - this is probably F2. April 7th: downcomer installed in LOX tank (which is almost fully stacked except for the thrust section). April 28th: Aft section finally taken inside High Bay 2 to have the rest of the LOX tank welded to it (which will complete the LOX tank stack). May 11th: Methane tank Forward section and the next barrel down taken into High Bay 2 and stacked. May 18th: Methane tank stacked onto another 3 ring next barrel, making it 9 rings tall out of 13. May 20th: Methane tank section stacked onto the final barrel, meaning that the Methane tank is now fully stacked. May 23rd: Started to install the grid fins. June 3rd: Methane Tank stacked onto LOX Tank, meaning that B11 is now fully stacked. Once welded still more work to be done such as the remaining plumbing and wiring.
B12
High Bay 2 (LOX Tank)
Under construction
June 3rd: LOX tank commences construction: Common Dome (CX:4) and a 4-ring barrel (A2:4) taken inside High Bay 2 where CX:4 was stacked onto A2:4 on the right side welding turntable. June 7th: A 4-ring barrel (A3:4) was taken inside High Bay 2. June 8th: Barrel section A3:4 was lifted onto the welding turntable and the existing stack placed on it for welding. June 9th: The next 4-ring barrel (A4:4) was taken inside High Bay 2, later in the day the incomplete LOX tank stack was hooked up to it and placed on the welding turntable for stacking and welding.
Are they replacing sheathing that was damaged during the first integrated flight test, or are they adding sheathing to part of the tower that never previously had sheathing?