Author Topic: SpaceX Starship : First Flight : Starbase, TX : 20 April 2023 - DISCUSSION  (Read 532645 times)

Offline Slothman

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I thought that gimbaling shot in the tweet from 44 minutes ago was current for a second but no. Pretty sure that's on a sub orbital mount.   

https://twitter.com/TrevorMahlmann/status/1647785292730884096

It is clearly the OLM. Note the pillar in the back and the piping up top
« Last Edit: 04/17/2023 03:01 am by Slothman »

Online FutureSpaceTourist

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https://twitter.com/thesheetztweetz/status/1647776673247506436

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Made my @NBCNightlyNews debut live from the Starship pad, to talk about one of the most significant rocket launches of the 21st century so far: https://www.nbcnews.com/nightly-news/video/spacex-s-starship-to-make-its-first-orbital-test-flight-170442821902


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twitter.com/sciguyspace/status/1647776508415471618

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It today the final day of the Before Starship Era? Because when this begins to work, it changes humanity’s relationship to the sky forever. Mass, volume, and cost have been ruthless adversaries to spaceflight. What happens when we start to beat them back? 🚀

https://twitter.com/rookisaacman/status/1647802583317381123

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We go to Mars

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« Last Edit: 04/17/2023 03:27 am by FutureSpaceTourist »

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https://twitter.com/jxck_sweeney/status/1647778084345757696

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Flights into Brownsville recently as Starship is posed to launch tomorrow. Elon Musk, Antonio Gracias (Fmr. Director of Tesla), and Yusaku Mazawa. Flying in from Tokyo, ~11 hour trip.

Online FutureSpaceTourist

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OMG

https://twitter.com/nasaspaceflight/status/1647805527378784256

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When the laser display folks like that we're enjoying their show, pop into chat, say "watch this,"- and put NSF on the Megabay for a few seconds..... 😎

nsf.live/starbase

Online FutureSpaceTourist

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https://twitter.com/hanskoenigsmann/status/1647828188423426048

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Good luck @SpaceX  and @elonmusk  🍀🚀

Offline sdfasdfasd

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re. The timing 2

Launch is now 8am at the earliest.
I guess Prop Load Go Poll is now 6am
Spacex video will begin at 7:15am
Starship splashdown is now 9:30am earliest

But is the launch window still 150 minutes or has it reduced to 90 minutes?

P.S. Can the orbit posts not simply be deleted by the mods when they appear?

Offline sanman

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Musk predictably downplaying expectations of a successful launch, while emphasizing the long-haul process:


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https://twitter.com/vickicocks15/status/1647866790955851782

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Here's a nice bit of info for you to mark the OFT of Starship today...Cryo Delivery numbers!
Total number of cryo deliveries since B7 Cryo (3rd Apr)
98 x LN2
32 x LOX
12 x CH4

Online FutureSpaceTourist

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https://twitter.com/SpacePadreIsle/status/1647876553018077185

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Huge line of vehicles at Isla Blanca Beach Park gate at 3am. Gate opens at 4am, Starship launch at 8am 🚀

Offline sanman

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Some guy from TimDodd/EDA's team asked Elon why no soft landing attempt for S24 at the end. Elon's reply seemed to say that he had such low expectations that S24 would achieve its full mission trajectory all the way, so that he didn't really care about attempting a soft landing (he also mentioned the inability to fit S24 with legs and ballast for tailsitter landing)

Offline sdfasdfasd

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Just listened to Musk's Starship Twitter Spaces discussion.

He mentioned the hundreds of changes from Booster 7 to Booster 9 including electric thrust vectoring, new heat shield, etc.

It occurred to me that that magnitude of change, to a rocket system that has already been designed and built, would take an Old Space company literally YEARS to plan, build, component test, integrate, integration test, etc etc. Really highlights the Move Fast And Break Things advantage.

Offline allio

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Regarding the booster return...

there has been no mention of an entry burn.... Is there not a risk of damage to the engines coming in hot without reducing speed. Falcon regulary knocks off 2000-3000 kph at entry burn.

any thoughts?

Offline CMac

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I understand that staging happens earlier, at lower speed. Also the steel can handle heat better

Offline allio

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I understand that staging happens earlier, at lower speed. Also the steel can handle heat better

It wasn't the steel i was worried about, rather the engines which take the brunt of it with the booster coming at the atmosphere ass first... If seperation is at a slower speed then apogee must be lower after boostback, thence reentry interface speed must be lower.

Any Numbers?

Offline Alvian@IDN

Regarding the booster return...

there has been no mention of an entry burn.... Is there not a risk of damage to the engines coming in hot without reducing speed. Falcon regulary knocks off 2000-3000 kph at entry burn.

any thoughts?
Electron recovery shows it's possible to survive what's Peter called "The Wall"
« Last Edit: 04/17/2023 10:09 am by Alvian@IDN »
My parents was just being born when the Apollo program is over. Why we are still stuck in this stagnation, let's go forward again

Offline CMac

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A lot of shipping out in the gulf along the debris path

Online FutureSpaceTourist

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https://twitter.com/spacerhin0/status/1647907988873572354

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Final look at what raptors we know on S24 and B7 ahead of their Orbital Launch Attempt!
(Now with new list-like descriptions)

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https://twitter.com/wapodavenport/status/1647922567649320960

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It’s a beautiful morning here on South Padre Island awaiting the launch of SpaceX’s Starship. A touch of the Milky Way over the rocket by ⁦@washpostnewton

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