SpaceX Falcon 9 Block 4 - SES-12 - Launching June 4, 2018
Screenshot of SpaceX Falcon 9 B4 - SES-12 with Tim Dodd as host
Mission Rundown: SpaceX Falcon 9 Block 4 - SES-12
Written: January 14, 2021
Connecting the dots of the orbit
SpaceX will launch a flight-proven Falcon 9 booster with a Block 5 second stage to put the SES-12 communication satellite into a geostationary transfer orbit. SES-12 is the heaviest payload ever launched to GTO by a Falcon 9 rocket at 5 384 kg.
The launch is scheduled for 12:45 a.m. EDT local time (4:45 UTC) on June 4th, 2018 in a four hour launch window out of SLC-40 at Cape Canaveral Air Force Station in Florida.
This first stage previously flew on the OTV-5 mission in September of 2017. There will be no attempt to recover the booster.
The Payload
SES-12 was designed and manufactured by Airbus Defence and Space. It has a mass of 5 383,85 kilograms (11 869,4 lb) and has a design life of at least 15 years.
Constructed by Airbus Defence and Space the satellite is built around a Eurostar E3000e platform – a variant of Airbus’ Eurostar 3000 product line that relies solely on its Russian designed SPT-140D thrusters as electric propulsion for orbit-raising and station keeping maneuvers. There are regular thrusters available as emergency avoidance thrusters.
The SES-12 satellite during radiotesting at Airbus
The SES-12 satellite expands SES's capabilities to provide direct-to-home (DTH) broadcasting, VSAT, Mobility, and High-Throughput Satellite (HTS) data connectivity services in the Middle East and the Asia-Pacific region, including rapidly growing markets such as India and Indonesia. The satellite replaces NSS-6 at this location and is co-located with SES-8 on 95.0° East. SES 12 is capable of supporting requirements in multiple verticals from Cyprus in the West to Japan in the East, and from Russia in the North to Australia in the South.
Together with SES-8, it reaches 18 million homes.
What did we learn today
Second stage is a Block 5 version, so SpaceX must be tweaking the second stage flight profile or fuel loading procedures. Anyway I assume the Block 5 second stage has a stronger thrust to weight ratio, since the Payload weighs 5 384 kg, and I assume that the previous second stage Block 3/4 model wouldn’t be able to do the GTO insertion to the same degree of satisfaction regarding the transfer orbits maximum apogee.
The picture above represents SES-12's seven month journey from its deployment in a Geostationary Transfer Orbit to its final Geostationary Orbit. Each dot is a burn using the onboard Hall Effect thrusters to raise its perigee - Blue dots, lower its apogee - Reed dots, and change the inclination - Green dots. It has been a long, slow trip for SES-12 since the Block 5 second stage deployed it on June 4th, 2018.
The spent second stage is now a derelict piece of space debris slowly deorbiting itself every time it reaches its perigee and experiences more and more drag from the upper atmosphere. It should deorbit within a couple of years.
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