Mission type | Communications |
---|---|
Operator | SES [1] |
COSPAR ID | 2016-013A |
SATCAT no. | 41380 |
Website | https://www.ses.com/ |
Mission duration | 15 years (planned) 8 years, 2 months, 2 days (elapsed) |
Spacecraft properties | |
Spacecraft type | Boeing 702 |
Bus | BSS-702HP [1] |
Manufacturer | Boeing |
Launch mass | 5,271 kg (11,621 lb) |
Start of mission | |
Launch date | 4 March 2016, 23:35 UTC |
Rocket | Falcon 9 Full Thrust |
Launch site | Cape Canaveral, SLC-40 |
Contractor | SpaceX |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | geostationary orbit |
Longitude | 108.2° East |
Transponders | |
Band | 33 Ku-band |
Bandwidth | 36 Mhz, 54 MHz |
Coverage area | Northeast Asia, South Asia, Indonesia |
SES-9 is a geostationary communications satellite operated by SES It was launched from Cape Canaveral SLC-40 by a Falcon 9 Full Thrust launch vehicle on 4 March 2016.
SES-9 is a large communications satellite operating in geostationary orbit at the 108.2° East, providing communications services to Northeast Asia, South Asia and Indonesia, maritime communications for vessels in the Indian Ocean, [2] and mobility beams for "seamless in-flight connectivity" for domestic Asian airlines of Indonesia and the Philippines. [3]
The satellite was built by Boeing, using a model BSS-702HP satellite bus. [4]
SES-9 had a mass of 5,271 kg (11,621 lb) at launch, [5] the largest Falcon 9 payload yet to a highly-energetic geosynchronous transfer orbit (GTO). [3] SES used the spacecraft's own propulsion capabilities to circularize the trajectory to a geostationary orbit. [6]
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 are on six Ku-band coverage beams: [7]
In addition to the earlier SES-8 mission ordered in 2011 and launched in 2013, SES contracted SpaceX for three additional launches starting with SES-9, originally planned for 2015. The deal was announced on 12 September 2012. [8] In early 2015, SES announced [9] that it would be the launch customer of the next rocket evolution by SpaceX: Falcon 9 v1.1 Full Thrust (also called Falcon 9 v1.2, [10] and later, just Falcon 9 Full Thrust). At the time, SES expected SES-9 to be launched by September 2015. [11] Despite the failure of the CRS-7 mission in June 2015, SES re-confirmed in September 2015 their decision to provide the first payload for the new rocket variant; however the launch was postponed until late 2015. [12]
Eventually, after considering all options, SpaceX announced a change on 16 October 2015: Orbcomm's 11 Orbcomm-OG2 satellites would be the payload on the return-to-flight mission of the redesigned rocket instead of SES-9. [11] The Orbcomm payload with its lower orbit would allow SpaceX to test relighting the second-stage engine, a capability required to successfully put the heavier SES-9 on a geostationary orbit. [11] The Orbcomm mission was subsequently delayed to mid-December 2015, while SES-9 was scheduled to follow "within a few weeks". [11] Finally, Falcon 9 Full Thrust performed its maiden launch on 22 December 2015, the final launch of the Falcon 9 v1.1 variant followed in January 2016, with SES-9 moving to February 2016. Consequently, this was the second launch of the Full Thrust variant. [4]
A successful static fire test of the rocket was completed on 22 February 2016. [4]
Attempt | Planned | Result | Turnaround | Reason | Decision point | Weather go (%) | Notes |
---|---|---|---|---|---|---|---|
1 | 24 Feb 2016, 11:46:00 pm | Delayed [13] | — | Issue loading cryogenic liquid oxygen | 60% | ||
2 | 25 Feb 2016, 11:47:00 pm | Aborted [14] | 1 day, 0 hours, 1 minute | Issue loading cryogenic liquid oxygen | (T-00:01:41) | 80% | |
3 | 28 Feb 2016, 11:47:00 pm | Aborted [15] | 3 days, 0 hours, 0 minutes | Fouled Range | 95% | ||
4 | 29 Feb 2016, 12:21:00 am | Aborted [15] | 0 days, 0 hours, 34 minutes | Low thrust alarm due to rising oxygen temps | 95% | ||
5 | 4 Mar 2016, 11:35:00 pm | Successful launch [16] | 4 days, 23 hours, 14 minutes | 90% | Launch window: 23:35 to 01:06 UTC |
The launch was initially scheduled for 24 February 2016 at 23:46 UTC, with a backup launch window the next day at the same time. [3] Neither day produced a launch however as both attempts were scrubbed: on 24 February 2016, prior to propellant loading "out of an abundance of caution, in order to get the rocket's liquid oxygen propellant as cold as possible"; and on 25 February 2016, just two minutes prior to launch "citing a last-minute problem with propellant loading". [17]
Subsequently, the launch was rescheduled for the evening of 28 February 2016 at 23:47 UTC, with a fallback slot same time next day. [18] On 28 February 2016, launch attempt was aborted less than two minutes before scheduled liftoff due to a tugboat entering the area of the offshore safety zone. [19] A second attempt on 28 February 2016 was made about 35 minutes later, after the downrange zone had been cleared, however, the rocket shut-down a moment after ignition due to low thrust flag from one engine. Rising oxygen temperature due to the hold for the tugboat to clear and a suspected helium bubble, the two are related: the helium bubble in the warmer LOX was affected by the earlier launch attempt, when the stage was pressurized (with helium) for some time, increasing the saturation of helium gas into the liquid oxygen, which could then bubble out when the turbopumps began rapidly drawing oxidizer from the tank for the launch (and lowering tank pressure in the zone around the turbopump inlet), were suggested by Elon Musk as the likely reasons for the alarm being triggered. [20] The next launch attempt on 1 March 2016 was postponed to 4 March 2016 due to high winds. [21]
The launch was finally attempted, and succeeded, on 4 March 2016 at 23:35:00 UTC. [6]
The original apogee for the transfer orbit contracted by SpaceX was 26,000 km (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 km (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,
External videos | |
---|---|
SES-9 Technical Webcast: Experimental Landing |
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, [22]
SpaceX confirmed in February 2016 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 (floating landing platform) named Of Course I Still Love You. [4] [23] [3] Although SpaceX successfully recovered a first booster on land following the December launch to a less-energetic orbital trajectory, [24] [25] they had not yet succeeded in booster recovery from any of the previous attempts to land on a floating platform. [23] 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. [22]
As expected, booster recovery failed: the spent first stage "landed hard", damaging the drone ship, [26] but the controlled-descent and atmospheric re-entry, as well as navigation to a point in the Atlantic Ocean over 600 km (370 mi) away [27] from the launch site, were successful and returned significant test data on bringing back a high-energy Falcon 9. [6]
The controlled descent through the atmosphere and landing attempt for each booster is an arrangement that is not used on other orbital launch vehicles. [28] SES CTO Martin Halliwell had informed SpaceX that they were willing to use the same rocket twice to power another satellite to orbit. [29] This idea became reality in March 2017 with the SES-10 mission flying with the reused booster from CRS-8.
By 21 March 2016, the hole in the deck of the drone ship had been nearly repaired. [30]
Ariane 5 is a retired European heavy-lift space launch vehicle developed and operated by Arianespace for the European Space Agency (ESA). It was launched from the Centre Spatial Guyanais (CSG) in French Guiana. It was used to deliver payloads into geostationary transfer orbit (GTO), low Earth orbit (LEO) or further into space. The launch vehicle had a streak of 82 consecutive successful launches between 9 April 2003 and 12 December 2017. Since 2014, Ariane 6, a direct successor system, is in development.
A launch vehicle is typically a rocket-powered vehicle designed to carry a payload from Earth's surface or lower atmosphere to outer space. The most common form is the ballistic missile-shaped multistage rocket, but the term is more general and also encompasses vehicles like the Space Shuttle. Most launch vehicles operate from a launch pad, supported by a launch control center and systems such as vehicle assembly and fueling. Launch vehicles are engineered with advanced aerodynamics and technologies, which contribute to high operating costs.
Falcon 9 is a partially reusable medium-lift launch vehicle that can carry cargo and crew into Earth orbit, designed, manufactured and launched by American aerospace company SpaceX. It can also be used as an expendable heavy-lift launch vehicle. The first Falcon 9 launch was on 4 June 2010. The first Falcon 9 commercial resupply mission to the International Space Station (ISS) launched on 8 October 2012. In 2020 it became the first commercial rocket to launch humans to orbit and remains the only such vehicle. It is the only U.S. rocket certified for transporting humans to the ISS. In 2022, it became the U.S. rocket with the most launches in history and with the best safety record, having suffered just one flight failure.
SES-8 is a geostationary Communications satellite operated by SES SES-8 was successfully launched on SpaceX Falcon 9 v1.1 on 3 December 2013, 22:41:00 UTC.
Orbcomm is a family of low Earth orbit communications satellites, operated by the United States satellite communications company Orbcomm. As of July 2014, 51 such satellites have orbited Earth, with 50 still continuing to do so.
Jason-3 is a satellite altimeter created by a partnership of the European Organisation for the Exploitation of Meteorological Satellites (EUMETSAT) and National Aeronautic and Space Administration (NASA), and is an international cooperative mission in which National Oceanic and Atmospheric Administration (NOAA) is partnering with the Centre National d'Études Spatiales. The satellite's mission is to supply data for scientific, commercial, and practical applications to sea level rise, sea surface temperature, ocean temperature circulation, and climate change.
Falcon Heavy is a partially reusable super heavy-lift launch vehicle that can carry cargo into Earth orbit, and beyond. It is designed, manufactured and launched by American aerospace company SpaceX.
SpaceX manufactures launch vehicles to operate its launch provider services and to execute its various exploration goals. SpaceX currently manufactures and operates the Falcon 9 Block 5 family of medium-lift launch vehicles and the Falcon Heavy family of heavy-lift launch vehicles – both of which are powered by SpaceX Merlin engines and employ VTVL technologies to reuse the first stage. As of 2024, the company is also developing the fully reusable Starship launch system, which will replace the Falcon 9 and Falcon Heavy.
SpaceX has privately funded the development of orbital launch systems that can be reused many times, similar to the reusability of aircraft. SpaceX has developed technologies over the last decade to facilitate full and rapid reuse of space launch vehicles. The project's long-term objectives include returning a launch vehicle first stage to the launch site within minutes and to return a second stage to the launch pad, following orbital realignment with the launch site and atmospheric reentry in up to 24 hours. SpaceX's long term goal would have been reusability of both stages of their orbital launch vehicle, and the first stage would be designed to allow reuse a few hours after return. Development of reusable second stages for Falcon 9 was later abandoned in favor of developing Starship, however, SpaceX developed reusable payload fairings for the Falcon 9.
SpaceX CRS-8, also known as SpX-8, was a Commercial Resupply Service mission to the International Space Station (ISS) which was launched on April 8, 2016, at 20:43 UTC. It was the 23rd flight of a Falcon 9 rocket, the tenth flight of a Dragon cargo spacecraft and the eighth operational mission contracted to SpaceX by NASA under the Commercial Resupply Services program. The capsule carried over 3,100 kilograms (6,800 lb) of cargo to the ISS including the Bigelow Expandable Activity Module (BEAM), a prototype inflatable space habitat delivered in the vehicle's trunk, which was attached to the station and, as of May 2022, is expected to remain so for five more full years of in-orbit viability tests.
Falcon 9 flight 10 was a Falcon 9 space launch that occurred on July 14, 2014. It was the fifth launch of the Falcon 9 v1.1 launch vehicle and carried six Orbcomm-OG2 telecommunication satellites. All six 172-kilogram-mass (379 lb) satellites were successfully deployed.
The Falcon 9 first-stage landing tests were a series of controlled-descent flight tests conducted by SpaceX between 2013 and 2016. Since 2017, the first stage of Falcon 9 missions has been routinely landed if the rocket performance allowed it, and if SpaceX chose to recover the stage.
Falcon 9 flight 20 was a Falcon 9 space launch that occurred on 22 December 2015 at 01:29:00 UTC. It was the first time that the first stage of an orbital rocket made a successful return and vertical landing.
SES-10, is a geostationary communications satellite awarded in February 2014, owned and operated by SES and designed and manufactured by Airbus Defence and Space on the Eurostar-3000 satellite bus. It is positioned at the 67° West position thanks to an agreement with the Andean Community to use the Simón Bolivar-2 satellite network. It replaces AMC-3 and AMC-4 to provide enhanced coverage and significant capacity expansion.
Falcon 9 Full Thrust is a partially reusable medium-lift launch vehicle, designed and manufactured by SpaceX. It was first designed in 2014–2015, with its first launch operations in December 2015. As of 7 May 2024, Falcon 9 Full Thrust had performed 311 launches without any failures. Based on the Laplace point estimate of reliability, this rocket is the most reliable orbital launch vehicle in operation.
Intelsat 35e, also known as IS-35e is an Intelsat high-throughput (HTS) geostationary communications satellite designed and manufactured by Boeing Satellite Systems on the Boeing-702MP satellite bus. It was launched on 5 July 2017.
Falcon 9 B1046 was a reusable Falcon 9 first-stage booster manufactured by SpaceX. It flew four times between 2018 and 2020 before it was expended during a successful abort test of the Crew Dragon. It was the first rocket of the final Falcon 9 upgrade, Block 5.
This mission is going to a Geostationary Transfer Orbit. Following stage separation, the first stage of the Falcon 9 will attempt an experimental landing on the "Of Course I Still Love You" droneship. Given this mission's unique GTO profile, a successful landing is not expected.
SES 9's launch weight is 5271 kg, [...] heavier than the Falcon 9 rocket's advertised lift capacity to geosynchronous transfer orbit, an elliptical path around Earth that serves as a drop-off point for communications satellites heading for positions 22,300 miles (35,900 kilometres) above the equator, a popular location for powerful broadcast platforms. Geosynchronous transfer orbits targeted by satellite launchers typically have an apogee, or high point, of at least 22,300 miles and a low point a few hundred miles above Earth. [...] SES's contract with SpaceX called for the rocket to deploy SES 9 into a "sub-synchronous" transfer orbit with an apogee around 16,155 miles (25,999 kilometres) in altitude. Such an orbit would require SES 9 to consume its own fuel to reach a circular 22,300-mile-high perch, a trek that Halliwell said was supposed to last 93 days. The change in the Falcon 9's launch profile [is planned to] put SES 9 into an initial orbit with an apogee approximately 24,419 miles (39,299 kilometres) above Earth, a low point 180 miles (290 kilometres) up, and a track tilted about 28° to the equator.
After a variety of problems delayed four previous launch attempts, a SpaceX Falcon 9 successfully launched the SES-9 communications satellite March 4, although an attempted landing of the rocket's first stage on a ship was not successful, as expected.
This mission also marks SpaceX's return-to-flight as well as its first attempt to land a first stage on land. The landing of the first stage is a secondary test objective.