Monday, January 6, 2014

SpaceX Falcon 9 - Thaicom 6

  SpaceX Falcon 9 V1.1 - Thaicom 6 - Launching January 6, 2014

Screenshot from SpaceX Webcast of the launch of Thaicom 6

Mission Rundown: SpaceX Falcon 9 V1.1 - Thaicom 6

Written: February 5, 2021

Lift Off Time

January 6, 2014 - 22:05:59 UTC - 17:06 EST

59 seconds are displayed on PAD clock at T+00:00:00

Mission Name

Thaicom 6

Launch Provider

SpaceX

Customer

Thaicom Public Company Limited

Rocket

Falcon 9 V1.1 serial number B1005

Launch Location

Space Launch Complex 40 - SLC-40

Cape Canaveral Air Force Station, Florida

Payload

Geostar-2 Communication Satellite

Payload mass

3 325 kg ~ 7 330 pounds

Where did the satellite go?

GEO Supersynchronous Transfer Orbit with initial range from 376 km - 90 039 km x 22,46° 

Will they be attempting to recover the first stage?

No. One way ticket flying “bareback” with no grid fins or landing legs + hydraulic tanks, pumps...

Where will the first stage land?

In the Atlantic ocean east of Florida

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:

– 8th flight of all Falcon 9 rockets

– 3rd flight of Falcon 9 V1.1 rocket

– 7th SpaceX launch from SLC-40

– 8th crash landing. Soft, hard, deliberate, ups...

– 1st mission for SpaceX in 2014

Where to watch

Where to read more

SpaceX don’t have much but dxrts link does

Have found a link from 169byg

Want to know or learn more link visit Tim Dodd


Launch debriefing

(This is what happend)

T-00:39:25

Hosts:

T 00:00:00

T+00:01:25

T+00:02:58

T+00:03:07

T+00:04:07

T+00:08:56

-

-

T+00:27:10

-

T+00:31:13

SpaceX live feed at 0:03

Molly McCormick, John Insprucker and Sarah Walker

Liftoff at 39:30 - 177/180 second burn time

MaxQ at 40:55

MECO 42:27, stage separation 42:29

SES-1 at 42:36 - 350 second burn time

Fairing separation confirmed at 43:37

SECO at 48:26 and coasting

Rap up from 49:44

SpaceX doesn't resumes live feed

SES-2 - SECO-2 in 60 seconds gave a velocity boost from 26 477 km/h to 36 136 km/h ish...

SpaceX doesn't show deployment - 17:57 EST



It’s colder up there, so why go GTO?

Thaicom 6 is a Thai television satellite of the Thaicom series, to be operated by Thaicom Public Company Limited (formerly Shin Satellite Public Company Limited), a subsidiary of Shin Corporation headquartered in Bangkok, Thailand. Thaicom 6 will be co-located with Thaicom 5 at 78.5 degrees East, ("Hot Bird" position), in geostationary orbit. The total cost for the satellite is US$ 160 million.

Thaicom 6 was launched on January 6, 2014, by Space Exploration Technologies Corp. on a Falcon 9 v1.1 launch vehicle. This is SpaceX's official business name. From the North West lightning tower the camera clock showed 17:03:58 EST with T-2:00 on the countdown clock, so it’s assumed that the launch was performed at 17:05:59 EST.

This launch was SpaceX' second payload to a Geostationary transfer orbit. Like the previous SES-8 launch, the Falcon 9 rocket injected Thaicom 6 into a supersynchronous GTO, from which SES-8 will complete its orbit maneuvers to the final geostationary orbit under its own power using a BT-4 apogee motor.

The Payload

THAICOM 6 (Thai: ไทยคม 6) is a Thai satellite of the Thaicom series, operated by Thaicom Public Company Limited, a subsidiary of INTOUCH headquartered in Bangkok, Thailand. THAICOM 6 is co-located with Thaicom 5 at 78.5 degrees East, in geostationary orbit. The total cost for the satellite is US$160 million.

THAICOM 6 is a 3-axis stabilized spacecraft, carrying 18 active C-band transponders and 8 active Ku-band transponders. The Ku-band transponders are both addressed as well as beam-switched to broadband. THAICOM 6 provides communication service to Southeast Asia, Africa and Madagascar with its primary role being DTH service for Thailand.

THAICOM 6 weighs 3.325 kg (7.330 pounds). It is based on a GEOstar bus built by Orbital Science Corporation, and gets 3,7 kW (5 hp) from its solar panels. Nothing more is mentioned about the satellite.

The spacecraft was launched on January 6, 2014, by SpaceX on a Falcon 9 v1.1 launch vehicle. The payload was delivered by SpaceX to a 90,000 kilometers (56,000 mi)-apogee supersynchronous elliptical transfer orbit that will later be reduced by the satellite builder Orbital Sciences Corporation to an approximately 35,800 kilometers (22,200 mi) circular geostationary orbit. The supersynchronous transfer orbit enables an inclination plane change with a lower expenditure of propellant by the satellite's small bipropellant kick motor.

This launch was SpaceX's second transport of a payload to a Geostationary transfer orbit. Both the SES-8 SpaceX launch before this and THAICOM 6 utilized a supersynchronous transfer orbit, but Thaicom 6 was at a somewhat greater apogee than that used for SES-8.

The Falcon 9 upper stage used to launch THAICOM 6 was left in a decaying elliptical low-Earth orbit which decayed over time and, on 28 May 2014, re-entered the atmosphere and burned up. Some 142 days and 324,6 orbits after the launch.

Space Launch Complex 40

Space Launch Complex 40 (SLC-40), previously Launch Complex 40 (LC-40) is a launch pad for rockets located at the north end of Cape Canaveral Space Force Station, Florida. Before the Amos-6 Pad failure this was known.

On April 25, 2007, the US Air Force leased the complex to SpaceX to launch the Falcon 9 rocket. SpaceX made a number of changes to the place. The Titan service tower was torn down, the ramp to the launch platform was altered to handle the Falcon 9 Transport Erector, aka. the strongback erector, which stands 200 feet high, when erected with a Falcon 9. Read more about SLC-40 here and here.

Two claws (arms) hold the rocket just under the payload, that either is the Dragon cargo supply capsule, or the payload fairing which can hold several satellites on the Payload Adapter Fitting - PAF placed just above the second stage top of its LOX tank. The Dragon uses a short turtleneck payload adapter to join the second stage round top to the earlike shape of the Dragon’s folded side mounted solar panels.

Around the launch pad there are four 250 feet high lightning towers with wires between them for extra safety. Under the launch pad is the flame trench, which diverts the flames, the smoke, the sound and the steam produced during liftoff by the 9 Merlin 1D engines at almost full throttle. Around at the base is a number of fire fighting waterspouts, who douse the rocket flames during liftoff.

During April 2008, construction started on the ground facilities necessary to support the launch of the SpaceX Falcon 9 rocket. Renovations included installation of new liquid oxygen tanks “size unknown'' and two 28.000 gallon kerosene tanks “106 cubic meters in each tank” and construction of a hangar for rocket and payload preparation.

The spherical liquid oxygen (LOX) tank was acquired from NASA. This spherical LOX tank was previously used at LC-34, where Apollo 1 met its demise, and it holds 110.000 gallon of LOX equal to 416,4 m3 or 475,1 ton LOX.

There are 6-7 railway cars with compressed Helium inherited from the Apollo/Titan era near the launch pad, and there are a number of Nitrogen gas tanks there as well. The most unusual tank is the N3 gas tank used in the Nitrogen Air Condition System ACS in the fairing, which keeps moisture, dust and corrosive air away from the payload.

I’m hearing the word “Nitrox” in the webcast, maybe I’m wrong about the above paragraph. Who knows for sure? I do know now. It is NitroLox that is used by divers and that means it's a pure moisture free artificial pressurized environment inside the fairings.

In total, 26 Titan IIIC, 8 Titan III(34)D, 4 Commercial Titan III, 5 Titan IVA and 12 Titan IVB rockets used SLC-40, with a total of 55 Titan rocket launches.

Just a grainy view of SLC-40 with SXM-8 from a Maxar satellite - Some sideway snapshot

LOX sphere and tanks close to the left. RP-1 tanks close to the right. TEL, the Falcon 9 and SXM-8 dead center. 4 square spaced lightning towers around the launch site. Helium and Nitrogen gas tanks behind the two left lightning towers. Storage and tool shed close by just behind the launch site and processing hangar with spare boosters to the far left.

Oh, and the black blast trench below the launch site. Water deluge Tower out of frame.

Author William Graham link

link

Coauthor/Text Retriever Johnny Nielsen

link to launch list


Tuesday, December 3, 2013

SpaceX Falcon 9 - SES-8

  SpaceX Falcon 9 V1.1 - SES-8 - Launching December 3, 2013

Screenshot from SpaceRef Business copy of SpaceX Webcast of the launch of SES-8

Mission Rundown: SpaceX Falcon 9 V1.1 - SES-8

Written: February 5, 2021

Lift Off Time

December 3, 2013 - 22:41 UTC - 17:41 EST

Mission Name

SES-8

Launch Provider

SpaceX

Customer

SES S. A.

Rocket

Falcon 9 V1.1 serial number B1004

Launch Location

Space Launch Complex 40 - SLC-40

Cape Canaveral Air Force Station, Florida

Payload

GEOStar-2.4 Communication Satellite

Payload mass

3 170 kg ~ 6 990 pounds

Where did the satellite go?

Supersynchronous Geostationary Transfer Orbit at 385 km x 79 113 km x 20,54° inclination

Will they be attempting to recover the first stage?

No. One way ticket flying “bareback” with no grid fins or landing legs + hydraulic tanks, pumps...

Where will the first stage land?

In the Atlantic ocean east of Florida

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:

– 7th flight of all Falcon 9 rockets

– 2nd flight of Falcon 9 V1.1 rocket

– 6th SpaceX launch from SLC-40

– 7th crash landing. Soft, hard, deliberate, ups...

– 3rd mission for SpaceX in 2013

Where to watch

Where to read more

SpaceX have very little video coverage

I found a link here with SpaceRef Business

Another link was found later with AATCCC

Want to know or learn more link visit Tim Dodd


Launch debriefing

(This is what happend)

T-00:15:07

Host:

T 00:00:00

T+00:01:24

T+00:02:57

T+00:03:07

T+00:04:01

T+00:08:27

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-

T+00:26:27

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T+00:33:27

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T-00:15:57

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T-00:13:00

T-00:00:38

T 00:00:00

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-

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SpaceRef Business live feed at 00:00

John Insprucker guiding us through a sunset launch

Liftoff at 15:08

MaxQ at 16:32

MECO 18:05, stage separation 18:07

SES-1 at 18:15

Fairing separation at 19:09 or 22:45:13 UTC

SECO at 23:35 and coasting

Rap up from 26:06

SpaceX doesn't resume live feed

SES-2 - SECO-2 in 77 seconds gave a velocity boost from 26 477 km/h to 36 136 km/h - real data unavailable

SpaceX doesn’t show deployment 5 minutes later

-----

AATCCC copy of webcast starts at 19:57 in video

Voice of John Insprucker hosting

GO - NO GO Poll by launch director

T+ flight clock disappeared at 35:25

Liftoff at 17:41:00 EST on Pad NW Timer

MECO at 38:48 - stage separation 38:52

SES-1 at 38:59

Fairing separation at 39:53

SECO at 44:47 - Maybe double audio report

Rap up from John Insprucker at 46:49



Let’s go higher - Geostationary Orbit

On December 3, 2013 SpaceX successfully completed its first geostationary transfer mission, with the Falcon 9 rocket delivering the SES-8 satellite to its targeted 295 x 80,000 km orbit. Falcon 9 executed a picture-perfect flight, meeting 100% of mission objectives.

SpaceX launched the SES-8 satellite this evening on a Falcon 9 rocket. Launch occurred as the window opened at 5:41 pm EST. Second stage reignition and burn was a success. The SES-8 spacecraft is now in a nominal GEO transfer orbit. So far it seems that the flight was completely nominal.

Falcon 9 lifted off from Space Launch Complex 40 (SLC-40) at 5:41 PM Eastern Standard Time. Approximately 185 seconds into flight, Falcon 9's second stage's single Merlin 1D vacuum engine ignited to begin a five minute, 20 second burn that delivered the SES-8 satellite into its parking orbit.

18 minutes after injection into the parking orbit, the second stage engine relith for just over one minute to carry the SES-8 satellite to its final geostationary transfer orbit. The restart of the Falcon 9 second stage is a requirement for all geostationary transfer missions.

Today's mission marked SpaceX's first commercial launch from its central Florida launch pad and the first commercial flight from the Cape Canaveral Air Force Station in over five years. SpaceX has nearly 50 satellite launches on manifest, of which over 60% are for commercial customers.

This launch also marks the second of three certification flights needed to certify the Falcon 9 to fly missions for the U.S. Air Force under the Evolved Expendable Launch Vehicle (EELV) program. When Falcon 9 is certified, SpaceX will be eligible to compete for all National Security Space (NSS) missions.

The Payload

The SES-8 satellite is built on the STAR-2.4 satellite bus by Orbital Sciences. It is the sixth satellite of that model to be built for SES.

The communications satellite is initially co-located at 95.0° East with NSS-6 in order to provide communications bandwidth growth capacity in the Asia-Pacific region, specifically aimed at high-growth markets in South Asia and Indo-China, "as well as provide expansion capacity for DTH, VSAT and government applications".

Specifications

  • Payload mass: 3,170 kilograms (6,990 lb)

  • Electrical power: 5 kW, using Gallium arsenide solar panels, and two 4,850 watt-hours (17,500 kJ) lithium-ion storage batteries

  • Battery backup: 4850 Watt-hour lithium-ion battery

  • SES-8’s propulsion system is a BT-4 monopropellant engine by IHI Corp.

  • 24 Ku band transponders as communications broadcasting payload

  • 1 small Ka band communications payload

  • 3 main reflector dishes - Two side and one center reflector

  • Service life: 15 years before allotted station keeping propellant runs out

A second burn of the upper stage was required, and was completed successfully, during the SES-8 mission in order to place the SES-8 tele communications satellite into the highly elliptical supersynchronous orbit for satellite operator SES from ground stations to effect a plane change and orbit circularization. 

The launch of SES-8 marks the first time SpaceX will deliver a satellite into geostationary transfer orbit, although it is not the first contract they have received to launch such a payload. Avanti Communications had previously ordered a Falcon 9 to deploy its Hylas-1 satellite, however following delays with the Falcon 9’s development this payload switched to an Ariane 5.

The SES-8 launch was the first commercial ComSat launch to occur from SLC-40 in 20 years, and the fourth such launch from the complex overall. The 3 previous commercial launches were all made by Commercial Titan III (CT-III) rockets; a hybrid of the Titan III(34)D and Titan IV aimed at the commercial geostationary launch market.

In the early hours of 1 January 1990, or late on 31 December 1989, a Commercial Titan III (CT-III) rocket carrying the Skynet 4A and JCSAT-2 communications satellites. The second and third Commercial Titan III each launched one Intelsat VI communications satellite.

The first, Intelsat VI F-3, failed to separate from the carrier rocket. It was eventually freed by means of jettisoning its perigee motor, leaving it stranded in low Earth orbit. Space Shuttle Endeavour retrieved the spacecraft during the STS-49 mission – a task which required three astronauts to perform a spacewalk – and attached a replacement kick motor before sending the satellite on its way to geostationary orbit. Later renamed Intelsat 603, the spacecraft was only retired from service earlier in the year 2013.

Space Shuttle Endeavour retrieved and repaired Intelsat VI F-3 during STS-49

The most recent commercial geostationary launch from SLC-40 was in June 1990, when the third Commercial Titan III orbited Intelsat VI F-4. Unlike the previous Intelsat launch, this mission was successful.

One further CT-III launch was made from SLC-40, however it carried a NASA payload; the Mars Observer mission to the red planet in September 1992.

A third deorbit burn failed, so the Falcon 9 upper stage used to launch SES-8 was left behind in a decaying elliptical low-Earth orbit which, by September 2014, had decayed enough and re-entered the atmosphere.

Author William Graham link

link

Coauthor/Text Retriever Johnny Nielsen

link to launch list


SpaceX - Eutelsat 36D

Screenshot from the launch of Eutelsat 36D. At last we get to see a normal GTO mission in daylight Mission Rundown: SpaceX Falcon 9 - Eutels...