Friday, March 4, 2016

SpaceX Falcon 9 - SES-9

  SpaceX Falcon 9 Full Thrust - SES-9 - Launching March 4, 2016

Screenshot from SpaceX Webcast of the launch of SES-9

Mission Rundown: SpaceX Falcon 9 FT - SES-9

Written: January 31, 2021

Lift Off Time

March 4, 2016 - 23:35 UTC - 18:35 EST

Mission Name

SES-9

Launch Provider

SpaceX

Customer

SES S. A.

Rocket

Falcon 9 Full Thrust serial number B1020

Launch Location

Space Launch Complex 40 - SLC-40

Cape Canaveral Air Force Station, Florida

Payload

BSS-702HP Communication Satellite

Payload mass

5 271 kg ~ 11 620 pounds

Where did the satellite go?

Geostationary Transfer Orbit - 323 km x 40 654  km

Will they be attempting to recover the first stage?

Yes - A drone ship are stationed east of SLC-40

Where will the first stage land?

OCISLY are waiting about 662 km downrange

Will they be attempting to recover the fairings?

No - Not expected to survive reentry or water impact

Are these fairings new?

Yes - Two Type 1 boat hull sized fairings - 34 x 17 feet with 10 evenly spaced ventilation ports in a circle

This will be the:

– 22nd flight of all Falcon 9 rockets

– 2nd flight of Falcon 9 Full Trust “V1.2” rocket

– 20th SpaceX launch from SLC-40

– 21st crash landing. Soft, hard, deliberate, Ups...

– 2nd mission for SpaceX in 2016

Where to watch

Where to read more

SpaceX link

Want to learn more link visit Tim Dodd

 

Launch debriefing

(This is what happend)

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SpaceX live feed at 00:33

Lauren Lyons, Michael Hammersley, Tom Praderio and John Insprucker are putting on a show this evening

TEA-TEB Ignition - Full Thrust check

Liftoff at 10:00

MaxQ at 11:23

MECO 12:39, stage separation 12:41

1st stage 0 - 8 325 km/h, 0 - 64,6 km, in 161 seconds

SES-1 at 12:49 - Velocity 8 209 km/h - 73,4 km

Faring separation at 13:41

Entry burn 16:37 by 3 Merlin 1D+ for 18 seconds

Landing burn 18:20 by 1 Merlin 1D+ for 21 seconds?

SECO at 18:56 - Velocity 26 981 km/h, 165 km

SpaceX resumes live feed at 36:32

Velocity drop by 549 km/h - Altitude increase 126 km

SES-2 - SECO-2 in 58 seconds gave a velocity boost from 26 432 km/h to 35 254 km/h at 37:03

Liquid oxygen sloshing about in LOX tank at 37:14

SpaceX show deployment at 42:07

Rap up from SpaceX at 42:52


How hard can water be?

SpaceX’s Falcon 9 rocket will deliver SES-9, a commercial communications satellite for SES, to a Geostationary Transfer Orbit (GTO).

SES S. A. is a world-leading satellite operator providing satellite-enabled communications services to broadcasters, Internet service providers, mobile and fixed network operators, and business and governmental organizations worldwide using its fleet of more than 50 geostationary satellites.

SpaceX is targeting an evening launch of SES-9 from Space Launch Complex 40 at Cape Canaveral Air Force Station, Florida. The approximately 90-minute launch window opens on March 4 at 11:35 pm UTC. The satellite will be deployed approximately 31 minutes after liftoff. If you want to know more, here’s another news source.

The Payload

SES-9 is a large communications satellite operating in geostationary orbit at 108.2° East, providing communications services to Northeast Asia, South Asia and Indonesia, maritime communications for vessels in the Indian Ocean and mobility beams for "seamless in-flight connectivity" for domestic Asian airlines of Indonesia and the Philippines.

The satellite was built by Boeing, using a model BSS-702HP satellite bus. SES-9 has 57 high-power Ku-band transponders, equivalent to 81 transponders of 36 MHz bandwidth and, co-located at 108.2°E alongside SES-7, it provides additional and replacement capacity for DTH broadcasting and data in Northeast Asia, South Asia and Indonesia, and maritime communications for the Indian Ocean. Broadcasts on six Ku-band coverage beams go to six different geographical areas in Asia.

SES-9 had a mass of approximately 5,271 kilograms (11,621 lb) at launch, the largest Falcon 9 payload yet to a highly-energetic geosynchronous transfer orbit (GTO). SES S.A. used the spacecraft's own propulsion capabilities to circularize the trajectory to a geostationary orbit.

SES-9 is a replacement for the NSS-11 satellite which was acquired by SES when it purchased GE Americom in 2001. Launched by a Proton-K/DM3 rocket in October 2000 with a design life of fifteen years, the satellite was initially named GE-1A, but following its acquisition by SES and the rebranding of GE Americom to SES Americom, it became Americom Asia-Pacific 1, or AAP-1.

The satellite was transferred to a new subsidiary, WorldSat, in January 2004 as WorldSat-1 and returned to SES Americom about a year later. In 2007, the satellite was transferred to another division, SES New Skies, as NSS-11. Following replacement by SES-9, NSS-11 will be relocated to a different orbital slot for further operation.

Risk Taking with Falcon 9

The original apogee for the transfer orbit contracted by SpaceX was 26,000 kilometers (16,000 mi), a subsynchronous highly-elliptical orbit that SES would then circularize and raise over several months before the satellite would be ready for operational service at 36,000 kilometers (22,000 mi). SES CTO Martin Halliwell indicated in February 2016 that SpaceX had agreed to add additional energy to the spacecraft with the launch vehicle and that a new apogee of approximately 39,000 km (24,000 mi) was the objective, in order to assist SES in the satellite becoming operational many weeks earlier than otherwise possible.

Following word from SES that SpaceX had allocated some of the normal propellant reserve margins for landing to placing the SES-9 satellite in a higher (and more energetic) orbit than originally planned, SpaceX confirmed in February that they would still attempt a secondary goal of executing a controlled-descent and vertical landing flight test of the first stage on the SpaceX east-coast Autonomous spaceport drone ship (a barge rebuilt as a floating landing platform) named Of Course I Still Love You.

Although SpaceX successfully recovered a first booster on land following the December launch to a less-energetic orbital trajectory, they had not yet succeeded in booster recovery from any of the previous attempts to land on a floating platform. Because the SES-9 satellite was very heavy and was going to such a high orbit, SpaceX indicated prior to launch that they did not expect this landing to succeed.

As expected, booster recovery failed: the spent first stage "landed hard", damaging the drone ship, but the controlled-descent and atmospheric re-entry, as well as navigation to a point in the Atlantic ocean over 600 kilometers (370 mi) away from the launch site, were successful and returned significant test data on bringing back a high-energy and fast flying Falcon 9 from a launch on SLC-40 in Florida.

The word “high-energy” means that the kinetic energy stored in Falcon 9’s velocity squared and multiplied by the first stage mass, and that is reduced by the air’s friction cubed, which makes a Falcon 9 first stage return look like a burning freight train coming down.

Hot, heavy and fast.

Author William Graham link

link

Coauthor/Text Retriever Johnny Nielsen

link to launch list


Sunday, January 17, 2016

SpaceX Falcon 9 - Jason-3

  SpaceX Falcon 9 V1.1 - Jason-3 - Launching January 17, 2016

Screenshot from SpaceX Webcast of the launch of Jason-3 in the fog

Mission Rundown: SpaceX Falcon 9 V1.1 - Jason-3

Written: February 1, 2021

Lift Off Time

January 17, 2016 - 18:42:18 UTC - 10:42:18 PST

Mission Name

Jason-3

Launch Provider

SpaceX

Customers

NOAA - National Oceanic and Atmospheric Administration

NASA - National Aeronautics and Space Administration

CNES - Centre National d'Etudes Spatiales

EUMETSAT - European Organization for the Exploitation of Meteorological Satellites

Rocket

Falcon 9 V1.1 serial number B1017

Launch Location

Space Launch Complex 4 East - SLC-4E

Vandenberg Air Force Base, California

Payload

Earth science satellite

Payload mass

553 kg ~ 1 219 pounds

Where did the satellite go?

Polar Low Earth Orbit - 1 328 km x 1 380 km by 66.05º

Will they be attempting to recover the first stage?

Yes - The Marmac 304 aka. JRTI has been rebuilt

Where will the first stage land?

Just Read The Instruction JRTI on the pacific ocean just some 279 km ~ 173 miles downrange

Will they be attempting to recover the fairings?

No - Not expected to survive reentry or water impact

Are these fairings new?

Yes - Two Type 1 boat hull sized fairings - 34 x 17 feet with 10 evenly spaced ventilation ports in a circle

This will be the:

– 21st flight of all Falcon 9 rockets

– 15th and last flight of Falcon 9 V1.1 rocket

– 2nd SpaceX launch from SLC-4E

– 20th crash landing. Soft, hard, deliberate, Ups...

– 1st mission for SpaceX in 2016

Where to watch

Where to read more

SpaceX link

Want to learn more link visit Tim Dodd


Launch debriefing

(This is what happend)


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SpaceX live feed at 00:21

Kate Tice, Brian Mahlstedt at Vandenberg, Tom Praderio and John Federspiel fumbling around in the fog

Liftoff at 21:49 - Rocket downlink delayed

MaxQ at 23:13

MECO 24:25, stage separation 24:30

SES-1 at 24:35 - Determined by flight telemetry

Faring separation at 25:07

Boost dogleg brake burn taking 30 seconds

Entry burn 28:50 by 3 Merlin 1D for 28 seconds

Landing burn 24:48 by 1 Merlin 1D for 21 seconds?

SECO at 30:55 and coasting

SpaceX resumes live feed at 1:14:52 - audio

SES-2 - SECO-2 in 9 seconds gave a velocity boost from 24 069 km/h to 25 117 km/h at 1:17:05

SpaceX don’t show deployment at 1:17:42

Rap up from SpaceX at 57:15

Mvac chilling heard at 7:21 pm on NASA Webcast

SES-3 deorbit burn at 7:22 pm EST

SECO-3 at 7:22 pm - With lift off at 5:42 pm


I can’t see. Where’s the lightswitch?

With this mission, SpaceX’s Falcon 9 rocket will deliver the Jason-3 satellite to low-Earth orbit for the U.S. National Oceanic and Atmospheric Administration (NOAA), National Aeronautics and Space Administration (NASA), French space agency Centre National d'Etudes Spatiales (CNES) and the European Organisation for the Exploitation of Meteorological Satellites (EUMETSAT).

The Jason-3 launch is targeted for a 18:42 UTC launch from Space Launch Complex 4E at Vandenberg Air Force Base, California. If all goes as planned, the Jason-3 satellite will be deployed approximately an hour after launch.

This mission also marks an experimental landing of the first stage on the SpaceX second drone ship named “Just Read the Instructions”. The landing of the first stage is a secondary test objective. Unfortunately one of the landing legs lockouts didn’t deploy, so the first stage tipped over and was destroyed. The wreck was brought back to port.

The Science Payload

Jason-3 will supply data for scientific, commercial, and practical applications to sea level rise, sea surface temperature, ocean temperature circulation, and climate change.

Jason-3 mission is to make measurements related to global sea surface height. When sea surface height is measured via altimetry, mesoscale ocean features are better simulated since the Jason-3 radar altimeter can measure precise global sea-level variations with very high accuracy. The scientific goal is to produce global sea surface height measurements every 10 days to an accuracy of less than 4 cm.

In order to calibrate the radar altimeter, a microwave radiometer measures signal delay caused by atmospheric vapors, ultimately correcting the altimeter's accuracy to 3.3 cm. This data is important to collect and analyze because it is a critical factor in understanding the changes in Earth's climate brought on by global warming as well as ocean circulation. NOAA's National Weather Service uses Jason-3's data to more accurately forecast tropical cyclones.

Jason-3 flies at the same 9.9-day repeat track orbit, this means Jason-3 will make observations over the same ocean point every 9.9 days. The orbital parameters are: 66.05º inclination, 1380 km apogee, 1328 km perigee, 112 minutes per revolution around Earth. Jason-3 is flying one minute behind Jason-2. The one minute time delay is applied in order to not miss any data collection between missions.

Jason-3 entered orbit about 15 miles (25 kilometers) below Jason-2. The spacecraft will gradually raise itself into the same 830-mile (1,336-kilometer) orbit and position itself to follow Jason-2’s ground track, orbiting a couple of minutes behind Jason-2. The two spacecraft will fly in formation, making nearly simultaneous measurements for about six months to allow scientists to precisely calibrate Jason-3’s instruments.

In the SpaceX launch Webcast it was stated that the LOX was not super chilled for easier loading of propellants. That means they are in the transition phase between different rocket types, and the Vandenberg launch facility was not ready for it. Or it means that the Falcon 9 V1.1 was not built to be loaded with RP-1 and superchilled LOX in a hurry.

Second stage deorbit burn

After hardley one orbit Falcon 9’s second stage was commanded to deorbit over the north pacific ocean near the american west coast. A large ocean area was declared a no go area in a NOTAM Notice To Airmen and Mariners in the north pacific ocean.

Notam area southeast of Hawaii used to deorbit the second stage after deployment of Jason-3

In the bottom right corner are the Notam area used for the launch of Jason-3 with a small black X - SpaceX - indicating Just Read The Instruction position, which is further to the west of the launch trajectory with a 66.05º inclination.

That required a shift of flight direction during the boost back burn, which I believe was one of the causes of booster B1017 demise including the fog at Vandenberg Air Force Base combined with the long LOX loading of Falcon 9. There was enough time to freeze everything over in a thick layer of ice including the leg lock latches.

The failure to lock one of the landing legs is the only reason that booster B10117 didn’t land properly as the only one of its production model V1.1. Alas it was not to be, B1017 tumbled over and destroyed itself on the barge deck of JRTI.

Second stage of this Falcon 9 launch usually delivers 75% of the work done on the payload before releasing the payload into its low earth polar orbit. The unsung heroes of SpaceX Falcon 9 launches are the second stages who with a single Merlin vacuum optimised rocket engine. In this case it's probably designated B2017, where B stands for booster, 2 stands for second stage and 017 is the production number on the second stage.

Nothing is certain about B2017 other than it deorbited after 140 minutes after barely one orbit southeast of Hawaii in the pacific ocean. For all I know the second stage booster could be launching out of number order. It's been known to happen for first stage boosters that they were launched out of numerical production order.

Author Willian Graham link

link

Coauthor/Text Retriever Johnny Nielsen

link to launch list


SpaceX - Eutelsat 36D

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