Is the adapter vulcanized rubber?Dreamchaser rides in a shroud, so no special adaptor needed beyond the usual to adapt any payload to the shroud.
Is the adapter vulcanized rubber?Dreamchaser rides in a shroud, so no special adaptor needed beyond the usual to adapt any payload to the shroud.
A line of #VulcanRocket boosters in final assembly. All destined for upcoming National Security missions. Decatur is becoming a juggernaut…
"The mission will explore the operational limits of Vulcan" - interesting! The ULA link doesn't really expand on that.
Mostly on the Centaur V side @torybruno?
The will be some maneuvers that help us more fully characterize Centaur
What will the test payload be?
CV= Centaur V.Inert steel plus some very interesting CV tech experiments
Is there a reason for that? Since this one is flying a mass simulator, would it be a good idea to have it fly on a 0 booster configuration, with a lighter dummy payload, in order to save the GEMs for another launch?
Partly because we could start with the CERT1 trajectory and add to that. This same time and allowed us to give DreamChaser just a little more time before switching
To the astonishment of absolutely nobody.The Pentagon’s Top Rocket Launcher Is Behind Profit Goals and Losing Staff
For over a decade, United Launch Alliance had an absolute monopoly. If the Pentagon wanted to send a spy satellite to space, the Boeing Co. and Lockheed Martin Corp. venture was its only choice.www.bnnbloomberg.ca
Judging by the fog,… I’d have to say this is Vandenberg SLC3 receiving a brand new 70k gallon (265k liter) liquid hydrogen tank for #VulcanRocket’s Centaur V. Together with the Atlas tank, the pad capacity has more than tripled to 100k gallons.
You mentioned activating the pad early next year. Will we see a Vulcan shipped out to Vandenberg earlier in the year to do fit checks/pad checkouts well in advance of the first west coast flight?
Since you guys liked the still so much, here’s a short video. #VulcanRocket
Hi Tory why is the CERT-2 launch delayed to October? If everything is ready why is it slipping for a month? Thank you
We wanted to put several technology experiments on board. Took a few extra days
View: https://twitter.com/ulalaunch/status/1837547596291739816Up she goes! Thought you might enjoy a #ToryTimeLapse of the encapsulated #Cert2 going atop #VulcanRocket
The second United Launch Alliance #VulcanRocket stands fully assembled for launch NET Oct. 4 on #Cert2 to fulfill flight test obligations and complete its certification process with the U.S. Space Force to carry national security payloads starting later this year.
Learn more in our blog:
Sep 24, 2024
A United Launch Alliance (ULA) Vulcan VC2S rocket will launch the second certification (Cert-2) mission from Space Launch Complex-41 at Cape Canaveral Space Force Station, Florida. The Cert-2 mission includes an inert payload and demonstrations associated with future Centaur V technologies. This is the second of two test flights required for ULA's certification process with the U.S. Space Force.
#Cert2 // Mission Profile
We are counting down to the first opportunity to launch #VulcanRocket on its #Cert2 flight test! Watch a preview video of what you can expect during the high-energy mission that will leave Earth orbit.
Watch on YouTube:
Hey Tory, I will be attending the launch on Friday. I understand that the window is from 6 am to 9 am. How long before launch will we have a targeted launch time?
Will their be a live stream?
Thanks for all you do.
Now: The targeted time is 6am (local). If there is lightning, a glitching instrument, or a stuck valve, etc, we can take time to sort that out and still launch as late as 9am.
Yes
Team Blue is looking forward to @ulalaunch’s Vulcan #Cert2 launch powered by two of our #BE4 engines! Each engine will produce 550,000 pounds of thrust. #PoweredByBE4
#Cert2 // ToryTalk
Learn from @ToryBruno what tomorrow’s #VulcanRocket launch is all about.
Solids...The Second flight of Vulcan hat little hickup
One of SRB lost it nozzle during ascent !
Vulcan just going on into space...
View: https://publish.twitter.com/?url=https://twitter.com/NASASpaceflight/status/1842169172932886538
One of two solid-propellant strap-on boosters provided by Northrop Grumman suffered an anomaly of some sort during the climb out of the lower atmosphere, but the Vulcan managed to continue on into orbit. What impact the issue might have on the Vulcan’s certification is not yet known, but ULA CEO Tory Bruno said it will be investigated.
“The trajectory was nominal throughout,” he said on the company’s launch webcast. “We did, however have an observation on SRB No. 1, so we will be off looking at that after the mission is complete.” No other details were provided.
@torybruno Do you have any info on the SRB anomaly that occurred at the start of the flight? Also Vulcan handled the asymmetric thrust so well, that was impressive! And an orbital bullseye!
View: https://twitter.com/torybruno/status/1842239927641129294Yes
Nozzle anomaly on SRM-1. Reduced and asymmetric thrust.
Rocket compensated, as designed.
Nominal trajectory. Bullseye insertion
No energetic events occurred.
Also, did you notice that the Centaur had to burn a full 20 seconds longer than normal to get its tiny mass simulator into orbit? I'd guess that translates to a failure to get a payload that's anywhere near the Vulcan's true payload capability anywhere near orbital speed today.
No. Standard reserves were adequate. Margins were not used
It has to have had a huge overcapacity for the core stage to be able to compensate for the thrust asymmetry after losing the nozzle. No way it could have achieved orbit with a full payload.
Incorrect
Good SRBs can be extremely reliable.I cannot help feeling the fact that the F9 doesn’t rely on SRBs is a distinct advantage.
On the positive side the BE-4s performed well again.
Glad to hear Tory! How much margin was there, with this being an inert payload?
If it would have been a heavier bird, would the same accuracy and precision still have been possible?
Yes
Sorry about the confusing terms on art.
All missions have propellant reserves
We add to that additional propellant margins based on the mass & the configuration of the rocket
Because this was compensated for within reserves, this anomaly was “invisible” to the rocket
And a fair bit of luck that the SRB burn-through wasn't toward the main stage...
Not a burn though
Looks pretty energetic
Yes, it looks dramatic, like all things on a rocket. But, it’s Just the release of the nozzle. No explosions occurred
Nozzle anomaly. Case and grain fine. Reduced, asymmetric thrust. Compensated for by booster
Again, not a case burn through.
As promised, here's a clip from one the new camera angles freshly cleared through ITAR.
string for extra drag?
A long, low release force harness that continues to collect data from the fairing after it has separated from the rocket. (this is the 51 foot fairing, for scale)
@torybruno what induces the oscillation seen in the fairing?
Forces from the separation system