Amazonas 4A

Last updated
Hispasat 74W-1
NamesAmazonas 4A, Amazonas 4
Operator Hispasat
COSPAR ID 2014-011A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 39616 OOjs UI icon edit-ltr-progressive.svg
Mission duration15 years
Spacecraft properties
Bus GEOStar-2
Manufacturer Orbital Sciences Corporation
Launch mass2,938 kg
Dry mass1,241 kg
Start of mission
Rocket Ariane 5 ECA
Launch site Kourou Space Center
Orbital parameters
Longitude73.9º W
Semi-major axis 42,164 km
Periapsis altitude 35,780.1 km
Apoapsis altitude 35,807.6 km
Inclination 0.1º
Period 1,436.1 minutes
Payload
24 Ku-band transponders
Amazonas 4 network
 

The Amazonas 4A, renamed in 2016 Amazonas 4 and since 2017 known as the Hispasat 74W-1, is a Spanish commercial communications satellite developed by Orbital Sciences Corporation and operated by Hispasat. It was successfully launched in 2014 and it is expected to have a service life of 15 years however, shortly after its launch the satellite suffered a power failure that limited its operability and life. [1]

Contents

It is positioned to cover all of South America and during its service life the satellite has offered coverage for some important events such as the 2016 Summer Olympics and World Cup football broadcasts. [2] [3]

Body

The satellite is based on the GEO Star-2.4 bus and has a dry mass of 1,241 kg. It is shaped like a square-faced prism 5 meters tall. Its lateral faces hold two deployable reflector-antennas and two retracting solar panels that, when fully deployed, give the satellite a diameter nearing 23 meters. [4] At launch, its mass was increased to 2,938 kg. [5]

Propulsion

The main engine is the bipropellant BT-4 developed by the Japanese company IHI Aerospace. It is fueled by unsymmetrical dimethylhydrazine using dinitrogen tetroxide as the oxidizer. The fuel is stored in spherical tanks pressurized with Helium.

The engine alone is 0.65 meters tall and has a dry mass of 4 kg while capable of producing 450 N of thurst. [6]

Attitude Determination & Control Subsystem

The attitude and control subsystem is state of the art employing a combination of electrically powered set of reaction wheels and chemical-inertial Hydrazine monopropellant thrusters in order to provide precise Earth-pointing capabilities.

Electrical Power Subsystem

The power requirements of the satellite are up to 4.8 kW although it was projected to support up to 6.2 kW. Those are provided by a combination of two independent arrays each composed by four panels featuring Ultra-Triple-Junction GaAs Solar cells and two 5,053 Watt-Hour Li-Ion batteries and avionics for power storage and distribution.

Communications Subsystem

The communications subsystem is the main payload of the satellite. It consists on 24 Ku-band transponders subdivided in two 15-for-12 groups of Linearized Channel Travelling Wave Tube Amplifiers (LCTWTAs). [7] In addition to two 2.5 x 2.7 meter single shell super elliptical deployable reflectors. All of them orientable and capable of working individually or grouped in order to speed up or relay communications. Nonetheless, a power failure in the electrical subsystem provoked the quick degradation of the subsystem and it has been speculated that, as a result, the satellite lost almost half of its communication potential being able to maintain only 12 of its transponders operational. In conjunction to the natural degradation of the solar panels in space, has greatly shortened the satellite's service life and its utility.

Its design signal strength lies between 46 and 48.5 dBW throughout all of South America. [8]

Launch

An Ariane 5 ECA rocket. Ariane 5 Mission 21.jpg
An Ariane 5 ECA rocket.

The satellite was launched the 22nd of March 2014, at 22:04 UTC, via an Ariane 5 ECA vehicle, from the Guiana Space Center in Kourou, French Guiana. [9] The launch was shared with the Astra 5B satellite. [10] [11] Amazonas 4A was successfully put into a GEO orbit of 35,807.6 km of apogee and 35,780.1 km of perigee, an inclination of 0.1º, a period of 1,436.1 minutes and a semi major maxis of 42,164 km. Since it was designed to cover all of South America, it initially operated on the longitude 61º W but since 2017 it has shifted to 73.9º W. [12] [13] [14] [15]

Power failure

Shortly after reaching its intended orbit the satellite suffered a partial power failure losing some of its capabilities and shortening its operational life.

The loss was estimated to halve the satellite's capabilities. [16] However, the difficulty in assessing the causes and severity of the failure forced Hispasat and the insurance company to open a joint investigation. It will remain open until the loss of the satellite, scheduled for 2029, but so far, the insured value has been estimated at 145 million euros. [17] [18] The economic impact of the power failure has been estimated on 11 million euros of lost income during for the first quarter of 2014 for Hispasat, with further 5.4 million euros lost in operating income. [19]

In addition, the incident provoked the scrapping of the high power companion satellite, the Amazonas 4B, replaced by the future Amazonas 5 and the two renamings the satellite has undergone. [20] [21]

Amazonas 4B

A preliminary agreement between Hispasat and Orbital Sciences Corporation was signed the 25th of June 2012. This agreement included the construction of two new satellites, Amazonas 4A and Amazonas 4B that will be located at orbital position 61 West longitude.

However, during 2014, in the wake of the partial power failure of the Amazonas 4A, the agreement was modified and the Amazonas 4B scrapped and replaced by the future project Amazonas 5. This time constructed by SSL. The Amazonas 5 was to provide the same capabilities of both the Amazonas 4A (previous to its power failure) and the Amazonas 4B. It was successfully put into orbit the 11th of September 2017.

Its planned specifications are not clear since it was cancelled before construction began. However, being projected together with the Amazonas 4A it is safe to assume that they would have been similar. Consequently, the Amazonas 4B was going to use the GEO Star-2.4 or the more modern GEO Star-3 as a bus. Its service life would have lasted about 15 years. It was projected that the engine would be the same as the Amazonas 4A: the BT-4 developed by the Japanese company IHI Aerospace. The communications subsystem was going to be the main payload of the satellite. It consisted of 18 Ku-band transponders, in addition to two 2.5 x 2.7 meter single shell super elliptical deployable reflectors.

See also

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References

  1. ↑ Satélite Amazonas 4A , retrieved 2021-07-10
  2. ↑ "Technical details for satellite AMAZONAS 4A". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2021-07-06.
  3. ↑ "Amazonas 4A readies for World Cup". advanced-television.com. 15 October 2013. Retrieved 2021-07-15.
  4. ↑ "Orbital-Built Amazonas 4A Commercial Communications Satellite Successfully Launched". Northrop Grumman Newsroom. Retrieved 2021-07-06.
  5. ↑ "Hispasat 74W-1". www.hispasat.com (in Spanish). Retrieved 2021-08-18.
  6. ↑ "Amazonas 4A – Spacecraft & Satellites" . Retrieved 2021-07-06.
  7. ↑ Robbins, Neal; Eze, David; Cohen, Helen; Zhai, Xiaoling; McGeary, William; Menninger, William; Chen, Morgan; Rodgers, Eddie (2018). "Space Qualified 200-Watt Q-band Linearized Traveling-Wave Tube Amplifier" (PDF). NASA. Archived (PDF) from the original on 2021-07-12.
  8. ↑ "Amazonas 4A → Amazonas 4 → Hispasat 74W-1". Gunter's Space Page. Retrieved 2021-07-06.
  9. ↑ "HISPASAT chooses Arianespace to launch its Amazonas 4A and AG1 satellites". Arianespace. Retrieved 2021-07-06.
  10. ↑ "Orbital-Built Amazonas 4A Commercial Communications Satellite Ready for Launch". www.businesswire.com. 2014-03-20. Retrieved 2021-07-10.
  11. ↑ "Ariane 5 Successfully Launches Astra 5B and Amazonas 4A Satellites". AmericaSpace. 2014-03-22. Retrieved 2021-07-10.
  12. ↑ "Real time satellite tracking for: AMAZONAS 4A". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2021-07-15.
  13. ↑ "Hispasat 74W-1 at 73.9°W - LyngSat". www.lyngsat.com. Retrieved 2021-08-18.
  14. ↑ "El satélite Amazonas 4 de HISPASAT completa el traslado a su nueva posición orbital en 74º Oeste". Hispaviación (in Spanish). 2017-12-21. Retrieved 2021-08-19.
  15. ↑ "El satélite Amazonas 4 cambia de posición y ofrecerá nuevos servicios sobre Brasil y Sudamérica". Avion Revue Internacional (in Spanish). 2017-12-21. Retrieved 2021-08-19.
  16. ↑ "Amazonas-4 major failure". advanced-television.com. 16 February 2015. Retrieved 2021-07-11.
  17. ↑ "Power System Failure Expected To Cost Amazonas 4A Half its Capacity, Prompt $100M Insurance Claim". SpaceNews. 2014. Retrieved 2021-07-10.
  18. ↑ Forrester, Chris (25 April 2014). "Hispasat's $100m claim on Amazonas 4A". advanced-television.com. Retrieved 2021-07-15.
  19. ↑ "Spaceflight Now | Breaking News | Power system failure detected on Amazonas 4A". www.spaceflightnow.com. Retrieved 2021-07-10.
  20. ↑ "Amazonas 4B". Gunter's Space Page. Retrieved 2021-07-11.
  21. ↑ "Hispasat". www.hispasat.com (in Spanish). Retrieved 2021-07-11.
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