Author Topic: SpaceX Falcon 9 : SXM-7 : CC SLC-40 : December 13, 2020 (17:30 UTC)  (Read 131395 times)

Online Steven Pietrobon

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T+8 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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Cutoff.

Touchdown!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online FutureSpaceTourist

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https://twitter.com/kyle_m_photo/status/1338176683250167808

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Beautiful liftoff of falcon 9 for SXM-7.  #SpaceX #Falcon9

Edit to add:

https://twitter.com/booster_buddies/status/1338178965924696064

Quote
And liftoff!
The @SpaceX lifts the @SIRIUSXM satellite into orbit.
The drone ship hosted a successful landing as well today.
« Last Edit: 12/13/2020 04:52 pm by FutureSpaceTourist »

Online Steven Pietrobon

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T+10 minutes. Upcoming events.

00:26:03 2nd stage engine restarts
00:26:47 2nd stage engine cutoff (SECO-2)
00:31:39 SXM-7 deployment
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online FutureSpaceTourist

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https://twitter.com/spacex/status/1338176923323658245

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Falcon 9’s first stage has landed on the Just Read the Instructions droneship

Online Steven Pietrobon

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Expected LOS Bermuda.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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T+15 minutes. Over the Atlantic Ocean.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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T+20 minutes. Heading towards Africa.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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AOS Gabon.

T+25 minutes. One minute and three seconds to second ignition which lasts for 44 seconds.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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Ignition!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Steven Pietrobon

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Cutoff!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online FutureSpaceTourist

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https://twitter.com/nasaspaceflight/status/1338181297831866371

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SES-2 complete. Nominal orbit insertion.
« Last Edit: 12/13/2020 04:58 pm by FutureSpaceTourist »

Online Steven Pietrobon

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T+30 minutes. One minute and 39 seconds to spacecraft deploy.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline cscott

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OCISLY.

T-10 minutes.
I think the announcer said this was JRTI when it landed.

Online Steven Pietrobon

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Separation!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Offline cscott

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A little bit more end-over-end rotation of the satellite there after deploy than I would have expected.

Online Steven Pietrobon

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25th launch this year. End of SpaceX coverage.

Congratulations to SpaceX and SiriusXM for the successful launch!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline ugordan

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25th launch this year.

... and only the 2nd launch where the booster was on its 7th flight if I'm not missing something. First for a non-Starlink customer, certainly.

I wonder if the customer got a huge discount on this or whether they're really confident in booster reuse. Good news either way.
« Last Edit: 12/13/2020 05:21 pm by ugordan »

Online Steven Pietrobon

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Looks like a sub-GTO flight requiring 2206 m/s to get to GSO. Spacecraft mass is about 7 t, while reusable GTO capability is 5.5 t, so as expected.

http://www.sworld.com.au/steven/space/speed.zip

SpaceX speed calculator by Steven S. Pietrobon. 4 May 2019.
Enter negative perigee height to exit program.
Enter negative final orbit for geosynchronous orbit.

Enter initial perigee height (km): 249
Enter SpaceX speed (km/h): 33682
Enter initial orbit inclination (deg): 27

Estimated inertial speed = 9786.7 m/s
Estimated apogee height = 19515.7 km

Enter required inclination change (deg): 27
Enter final orbit height (km): -1
Geosynchronous altitude = 35786.0 km

Burn at   249.0 km: theta1 =  0.00 deg, dv1 =  409.1 m/s
Burn at 35786.0 km: theta2 = 27.00 deg, dv2 = 1800.3 m/s
dv = 2209.4 m/s

Burn at   249.0 km: theta1 =  0.29 deg, dv1 =  412.2 m/s
Burn at 35786.0 km: theta2 = 26.71 deg, dv2 = 1794.1 m/s
dv = 2206.3 m/s
« Last Edit: 12/13/2020 05:32 pm by Steven Pietrobon »
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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