Author Topic: Firefly Alpha FLTA004 : Tantrum : VSFB SLC-2W : 22 Dec 2023 (17:32 UTC)  (Read 42118 times)

Offline ZachF

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Sadly, Celestrak data (https://celestrak.org/NORAD/elements/table.php?INTDES=2023-202) seem to indicate that atmospheric drag is winning.

The Celestrak data looks to me like there is ONLY a slow orbital decay happening.
I don't see evidence for any significant spacecraft thrusting taking place- or if any is, as you note drag is winning.

Something to remember with orbit decay is that the rate of decay speeds up exponentially as altitude decreases.
« Last Edit: 12/26/2023 09:54 pm by ZachF »
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Offline sdsds

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Something to remember with orbit decay is that the rate of decay speeds up exponentially as altitude decreases.

Yes, there's certain to be a non-linearity in there somewhere! Someone with expertise and experience could probably quantify that.

Meanwhile it's relatively fun and easy to calculate wrong results via linear extrapolation. Using two recent data points from Celestrak the eccentricity would drop to zero on Valentine's Day, at which point the circular orbit would be at something like 160 km, which wouldn't last long. So Feb 14, 2024 looks like the No Later Than date for re-entry.

A slightly more realistic approach (though still wrong) derives from the observation that at the initial perigee height of 211 km the spacecraft was experiencing significant drag. When the SMA reaches that height the data would likely start really showing the knee in the curve and the satellite would be truly doomed. Extrapolating from the recent SMA datapoints, that would be Feb 1, 2024.

Repeating for emphasis: these aren't even really guesses since they are almost certainly wrong.
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Offline Steven Pietrobon

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A belated post of the Tantrum online press kit.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline VLN

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Can anyone explain what’s going on here?
Is this change of slope of SMA due to a real ongoing transfer of orbital energy from B to A?
Or is it an artifact of how Celestrak plots SMA (as altitude rather than apogee and perigee separately)?
Anyway, the plot seems to suggest that A (presumably the Lockheed ESA payload) will last a tad longer than previously expected.

Offline deltaV

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Can anyone explain what’s going on here?
Is this change of slope of SMA due to a real ongoing transfer of orbital energy from B to A?
Or is it an artifact of how Celestrak plots SMA (as altitude rather than apogee and perigee separately)?
Anyway, the plot seems to suggest that A (presumably the Lockheed ESA payload) will last a tad longer than previously expected.

My guess is nothing physically happened but the software that decides which radar returns belong to which object had a bad day and swapped the two objects for the last point in time. If you plot object B's last SMA and eccentricity on object A's plot and vice versa the last point in time continues the trend lines.

Online jcm

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Can anyone explain what’s going on here?
Is this change of slope of SMA due to a real ongoing transfer of orbital energy from B to A?
Or is it an artifact of how Celestrak plots SMA (as altitude rather than apogee and perigee separately)?
Anyway, the plot seems to suggest that A (presumably the Lockheed ESA payload) will last a tad longer than previously expected.

My guess is nothing physically happened but the software that decides which radar returns belong to which object had a bad day and swapped the two objects for the last point in time. If you plot object B's last SMA and eccentricity on object A's plot and vice versa the last point in time continues the trend lines.


It's very common for Space Force to swap the identities of objects without telling anyone.
I have no doubt that is what has happened in this case. Likely they have decided the old B object was actually the payload, so they have changed its identity to A and vice versa

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Offline PM3

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58616   TYVAK-1015 (TANTRUM)  2023-202A   140.01   501   214
58617   FIREFLY ALPHA R/B     2023-202B   140.02   487   210
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Offline sdsds

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Ignoring the glitch datapoint it still looks pretty linear....
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Offline VLN

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It's been a while, and the assignments of tracking data to Tantrum and its rocket booster appear to have swapped a couple more times. Both also show a clear sign of accelerating orbital decay: not just a steady decline of SMA but also a bend downward, a progressively steeper slope. This suggests that reentry is near.

I was able to download the plot data as CSV, and did my best to unswap them starting with today's data and and assignments, and working back toward launch day. I also applied a linear operation on the SMA and ellipticity to derive separate apogee and perigee altitudes.

The perigee trace of 58617 (R/B) shows an accelerating decline, clearer than its apogee trace, and clearer than 58616 (Tantrum payload). The sharpness of the downturn appears to me to indicate booster re-entry in the next week or so.

The perigee of 58616 (Tantrum) also shows a discernible acceleration of its decline. After some curve fitting and extrapolation, I offer a guess of three weeks (first week of Feb) for its reentry.

Note that my plots use different vertical scales for apogee and perigee.

I have only been playing with polynomial fits and inflection points to come to these conclusions. I acknowledge the lack of traditional physics and methods, and that's why I spoke vaguely in terms of weeks.

Offline sdsds

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Celestrak reports the Firefly upper stage re-entered; the payload is still orbiting.
— 𝐬𝐝𝐒𝐝𝐬 —

https://spacenews.com/lockheed-martins-misplaced-satellite-to-fall-back-to-earth-next-month/

Quote
ORLANDO, Fla. — A Lockheed Martin satellite that was placed in the wrong orbit Dec. 22 is expected to de-orbit in February. Despite a much shortened mission, the company said it successfully accomplished many of the objectives of the technology demonstration.
...
Bob Behnken, director of technology acceleration at Lockheed Martin Space, told SpaceNews in a statement that the company’s antenna technology demonstration payload “exceeded our expectations and successfully completed all primary mission objectives. This feat is even more impressive in light of the spacecraft being placed in an unplanned, lower orbit, which resulted in a dramatically compressed mission timeline.”
...
From the lower orbit location, he said, “we’ve completed more than 100 payload testing events to date, and continue to achieve more each day.”

edit/gongora: trimmed, do not post copyrighted articles in their entirety
« Last Edit: 01/31/2024 08:50 pm by gongora »

Offline Ken the Bin

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Firefly updated their mission webpage sometime on January 31 with a statement from the CEO. Unfortunately it's just fluff.

https://fireflyspace.com/missions/fly-the-lightning/

Quote from: Firefly
January 31, 2024

“As Firefly communicated in the immediate hours following Alpha FLTA004, we experienced a mishap when the second stage failed to achieve the planned target orbit for payload deployment. The subsequent investigation is progressing very well, and we will have more information to share in the weeks ahead as we wrap up our review and take corrective action. As part of that process, we invited our mission partner and future customers to serve as external oversight of the investigation for full transparency, and that exchange has been extremely valuable for the entire community.

Despite these challenges, the Firefly team placed our mission partner in an orbit where they successfully completed their primary mission objectives, including rapid commissioning of the satellite following insertion.  Before communicating any further mission-related status on our partner’s payload, we waited until their confirmation of performance and success, which they released in a recent statement.

Ultimately, the important long-term outcome is the rapid, thorough maturation of Alpha as the dependable one metric ton class rocket the market is demanding, which Firefly is dedicated to and is delivering. In the near term, it is a testament to the hard work and commitment of Firefly as a company that we were able to work alongside our partner to achieve this positive outcome.” – Bill Weber, CEO of Firefly Aerospace

Offline sdsds

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[...] So Feb 14, 2024 looks like the No Later Than date for re-entry.

The knee in the curve is now evident.
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Offline GewoonLukas_

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Quote
Tantrum reported to have reentered sometime between 1426 and 1518 UTC Feb 10. That almost 1 hr uncertainty corresponds to a track from Brazil to S Africa to NW Australia to Papua to Wake Island.

https://twitter.com/planet4589/status/1756696249875472615
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Offline VLN

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https://spacenews.com/lockheed-martins-misplaced-satellite-to-fall-back-to-earth-next-month/

Quote
ORLANDO, Fla. — A Lockheed Martin satellite that was placed in the wrong orbit Dec. 22 is expected to de-orbit in February. Despite a much shortened mission, the company said it successfully accomplished many of the objectives of the technology demonstration.
...
Bob Behnken, director of technology acceleration at Lockheed Martin Space, told SpaceNews in a statement that the company’s antenna technology demonstration payload “exceeded our expectations and successfully completed all primary mission objectives. This feat is even more impressive in light of the spacecraft being placed in an unplanned, lower orbit, which resulted in a dramatically compressed mission timeline.”
...
From the lower orbit location, he said, “we’ve completed more than 100 payload testing events to date, and continue to achieve more each day.”

edit/gongora: trimmed, do not post copyrighted articles in their entirety
The payload maker & operator claims 100% success for their mission, despite the failure to reach the intended orbit. It seems to me that makes the Firefly Alpha FLTA004 mission success close to 100% also, because of the fortuitously relaxed needs of the customer.

Of course, we also hope Firefly will be able sort out the second stage problem so that a normal customer mission can be fully satisfied.

Offline edkyle99

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The payload maker & operator claims 100% success for their mission, despite the failure to reach the intended orbit. It seems to me that makes the Firefly Alpha FLTA004 mission success close to 100% also, because of the fortuitously relaxed needs of the customer.
With all due respect.  No.

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Offline eeergo

The payload maker & operator claims 100% success for their mission, despite the failure to reach the intended orbit. It seems to me that makes the Firefly Alpha FLTA004 mission success close to 100% also, because of the fortuitously relaxed needs of the customer.

Of course, we also hope Firefly will be able sort out the second stage problem so that a normal customer mission can be fully satisfied.

Would you claim 100% success for a package delivery truck that broke down a ways away from the intended parcel recepient, dropping it into a neighbor's swimming pool in the process... just because the box happened to contain chlorine tablets for water cleaning, and the original recepient was a nearby convenience store who would be selling them to the pool's owner anyway?

It's pretty much the same situation, if you think about it.
-DaviD-

Online Galactic Penguin SST

https://twitter.com/firefly_space/status/1759950982908117051

Quote
Our dedicated team has completed the flight data review for Alpha FLTA004 and determined root cause after Alpha’s second stage did not achieve the target orbit for payload deployment. With corrective actions underway, Alpha will be ready to fly again in the coming months. Learn more here: https://fireflyspace.com/missions/fly-the-lightning/

Quote
…The investigation determined the mishap was due to an error in the Guidance, Navigation, and Control (GNC) software algorithm that prevented the system from sending the necessary pulse commands to the Reaction Control System (RCS) thrusters ahead of the stage two engine relight.



… Firefly is now implementing corrections actions to ensure the GNC software issue is resolved, including process changes to detect and prevent similar issues in the future. Alpha will be ready to fly again in the coming months.
« Last Edit: 02/20/2024 01:46 pm by Galactic Penguin SST »
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Online catdlr

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just adding a comment to the above post

https://twitter.com/DJSnM/status/1759954805584203955

Quote
Software again - writing reliable code is hard.
So my question is, were the RCS commands supposed to perform propellant settling, and the engine didn’t fire, or was it supposed to set/stabilize attitude, meaning engine fire was in the wrong direction?
« Last Edit: 02/20/2024 04:55 pm by catdlr »
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Online JohnLloydJones

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just adding a comment to the above post

https://twitter.com/DJSnM/status/1759954805584203955

Quote
Software again - writing reliable code is hard.
So my question is, were the RCS commands supposed to perform propellant settling, and the engine didn’t fire, or was it supposed to set/stabilize attitude, meaning engine fire was in the wrong direction?

Retired software guy here and yes, reliable software can be hard. but it can be done. With the necessary time and money, of course. Mostly comes down to the company culture. I'm afraid.

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