In the year 1989, Motorola announced a proposal to launch a series of 77 satellites in low Earth orbit starting in the year 1994. In the year 1992, a frequency spectrum between 1610 and 1626.5 MHz was allocated for the use by LEO satellites.
When we say Low Earth Orbit (LEO, it refers to a satellite which orbits the earth at altitudes between (very roughly) 200 miles and 930 miles. Its satellites must travel very quickly to resist the pull of gravity approximately 17,000 miles per hour. Because of this, Lowe Earth Orbit satellies can orbit the planet in as little as 90 minutes.
Low Earth Orbit satellite systems require several dozen satellites to provide coverage of the entire planet. Low Earth Orbit satellites typically operate in polar orbits. Low Earth Orbit satellites are used for applications where a short Round Trip Time (RTT) is very important, such as Mobile Satellite Services (MSS). Low Earth Orbit satellites have a typical service life expectancy of five to seven years.
Objects in LEO encounter atmospheric drag in the form of gases in the thermosphere (approximately 80–500 km up) or exosphere (approximately 500 km and up), depending on orbit height. LEO is an orbit around Earth between the atmosphere and below the inner Van Allen radiation belt. The altitude is usually not less than 300 km because that would be impractical due to the larger atmospheric drag.
BillikenSat-II will be operating in Low Earth Orbit, at around 700 km altitude. In this environment, both infrared radiation and albedo (reflected solar energy) must be taken into consideration, along with the direct solar radiation. These forms of radiation, represented graphically below, are the only sources of heat for the satellite since it is operating in the vacuum of space. As you may know, heat is transferred via convection, conduction, or radiation. Radiation is the main mode of heat transfer in space because it requires no medium and is actually more efficient in a vacuum. Because there is no air either in space or the main structure of the satellite, convection plays no part in the thermal environment. Conduction is important when analyzing the heat transfer from the main structure to the internal components.
Typical Low Earth Orbit (LEO) satellite temperatures can range from -40o Celsius to 85o Celsius, but depend largely on the orbital characteristics as well as the materials used in the spacecraft, in addition to heat generated by internal components (such as micro processors) and active thermal control.
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LEO Satellite Cell Structure |
Benefits of the LEO concept
- LEOs can offer a communications infrastructure to areas where there is insufficient population to justify a terrestrial based cellular network. This not only includes many developing countries but 80% of the US as well. This explains why most of the initiatives for LEOs has come from the USA.
- Many developing countries are interested in LEO systems as an alternative to investing in an very expensive terrestrial tele-communications infrastructure.
- Communication via LEOs does not suffer from the objectionably long transmission delays associated with geosynchronous systems.
- User equipment does not require high-power transmitters or highly directional antennae that need to be continually pointed to the satellite. In practice, transmit powers can be much lower than 1 watt.
- LEO satellites, are technically much simpler and more robust than geo-synchronous satellites and are less likely to suffer catastrophic failure during deployment or during the satellite lifetime.
LEOS and their advantages
LEO satellites are small communications transceivers. They are put in continuous motion at heights of 500-1200 miles above the earth. LEOS can provide 100 percent geographic coverage, LEO systems require less power for messages to reach their orbiting satellites , making it possible for specialised portable phones to transmit signals directly to the satellites. This makes phone calls independent of land based servers; allowing people to be reached anywhere in the world. Furthermore, less power requirements translate into lower service and equipment costs for users.
A major problem facing LEOS
Over 35 million bits of debris primarily pieces of old satellites, launch vehicles and solid rocket fuel currently orbit the earth, at speeds of up to seven kilometers per second. In comparison, a bullet fired from a high-speed rifle travels at only 0.8 kilometers per second. This forces LEO companies such as Iridium and Globalstar to worry not only about making sure their satellites work but that flying garbage doesn't knock them out of commission. Studies conducted by the National Aeronautics and Space Administration show that a collision with a fragment the size of a marble would do serious damage to a satellite. A 10 centimeter piece would be enough to permanently put the satellite out of order.
ConclusionDespite impediments and problems , LEOS still have many advantages over GEOS . Most important of which they are not confined by ground coverage of cellular phone relays , allowing people to communicate anywhere at any time . In the near future most human communication will be made through low earth orbiting satellites . Companies such as Iridium have already constructed a bridge to that future .
Reference:
- http://www.tech-faq.com/low-earth-orbit.html
- http://www.collegetermpapers.com/TermPapers/Technology/low_earth_orbit_satellites.shtml
- http://www.gare.co.uk/technology_watch/leo.htm