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APSTAR-6E
Technical Specifications
DFH-3E BUS The Dong Fang Hong 3E (DFH-3E) Bus is a satellite platform developed by the China Academy of Space Technology (CAST). It is a part of the DFH satellite series, known for its reliability and adaptability for various space missions. FeaturesHigh Payload Capacity: The DFH-3E Bus can carry multiple payloads, making it suitable for complex missions requiring various instruments. Power Supply: Equipped with efficient solar arrays and batteries, it provides a reliable power supply to onboard instruments. Propulsion System: Includes advanced propulsion technology for orbit insertion, station-keeping, and maneuvers. Modular Design: The platform’s modular architecture allows for customization based on mission requirements, facilitating the integration of different types of payloads. Enhanced Communication: It supports high-bandwidth communication capabilities, essential for data-intensive applications like remote sensing and telecommunications. Stability and Control: Advanced attitude control systems ensure the stability and precise orientation of the satellite, crucial for accurate data collection and transmission. |
Capabilities and Services
Innovation
Operational Goals
Different Types of Propulsion Systems used in Satellites
Type of Propulsion System |
Description |
Advantages |
Disadvantages |
Chemical Propulsion |
Uses chemical reactions to produce thrust (e.g., bipropellant or monopropellant systems). |
High thrust, quick maneuvering, reliable. |
Limited fuel supply, higher mass, more complex handling. |
Electric Propulsion |
Uses electric or magnetic fields to accelerate ions or plasma (e.g., ion thrusters, Hall effect). |
High efficiency, longer operational life, lower fuel mass. |
Low thrust, long time to achieve high speed, complex technology. |
Cold Gas Propulsion |
Expels inert gas through a nozzle to produce thrust. |
Simple design, safe, reliable. |
Very low efficiency and thrust, limited to small maneuvers. |
Solar Sail Propulsion |
Uses radiation pressure from sunlight on large reflective sails to produce thrust. |
No propellant needed, potentially unlimited range. |
Very low thrust, large area required, slow acceleration. |
Nuclear Thermal Propulsion |
Uses nuclear reactions to heat a propellant that is then expelled to produce thrust. |
High efficiency and thrust, long missions possible. |
Complex technology, safety concerns, political and regulatory issues. |
Hybrid Propulsion |
Combines features of chemical and electric propulsion systems to optimize performance. |
Balances thrust and efficiency, adaptable for various missions. |
Complex design, integration challenges, potential reliability issues. |
Satellites Using Electric Propulsion
Satellite |
Launch Date |
Operator |
Platform |
Electric Propulsion Type |
Primary Mission |
APSTAR-6E |
January 13, 2023 |
APT Satellite |
DFH-3E |
Ion thrusters |
High-throughput broadband services in Asia-Pacific |
SES-12 |
June 4, 2018 |
SES S.A. |
Eurostar E3000e |
Hall effect thrusters |
Direct-to-home TV and broadband in Asia-Pacific and Middle East |
Eutelsat 172B |
June 1, 2017 |
Eutelsat |
Eurostar E3000e |
Hall effect thrusters |
Broadband, mobility, and data services in Asia-Pacific |
Intelsat 29e |
January 27, 2016 |
Intelsat |
EpicNG |
Hall effect thrusters |
High-throughput services across the Americas and North Atlantic |
GOES-R Series |
November 19, 2016 |
NOAA/NASA |
A2100 |
Ion thrusters |
Weather forecasting and environmental monitoring |
Koreasat 5A |
October 30, 2017 |
KT SAT |
Spacebus 4000B2 |
Electric propulsion (Xenon) |
Direct-to-home broadcasting and broadband |
Boeing 702SP |
February 1, 2015 |
ABS, Eutelsat |
Boeing 702SP |
Ion thrusters |
Telecommunications |
ViaSat-2 |
June 1, 2017 |
ViaSat Inc. |
Boeing 702 |
Ion thrusters |
High-speed satellite internet |
JCSAT-14 |
May 6, 2016 |
SKY Perfect JSAT |
Spacebus 4000C4 |
Electric propulsion (Xenon) |
Telecommunications |
SES-15 |
May 18, 2017 |
SES S.A. |
Boeing 702 |
Electric propulsion (Xenon) |
High-throughput services across the Americas |
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PRACTICE QUESTION Q: With reference to the APSTAR-6E satellite, consider the following statements:
Which of the statements given above is/are correct? (a) 1 and 2 only (b) 2 and 3 only (c) 1 and 3 only (d) 1, 2, and 3 Answer: (c) |
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