Английская Википедия:Interstellar Probe (1999)

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Interstellar Probe is the name of a 1999 space probe concept by NASA intended to travel out 200 AU in 15 years.[1] This 1999 study by Jet Propulsion Laboratory is noted for its circular 400-meter-diameter solar sail as a propulsion method (1 g/m2) combined with a 0.25 AU flyby of the Sun to achieve higher solar light pressure, after which the sail is jettisoned at 5 AU distance from the Sun.[2]

Solar sail

Solar sails work by converting the energy in light into a momentum on the spacecraft, thus propelling the spacecraft.[3] Felix Tisserand noted the effect of light pressure on comet tails in the 1800s.[3]

The study by the NASA Jet Propulsion Laboratory proposed using a solar sail to accelerate a spacecraft to reach the interstellar medium. It was planned to reach as far as 200 AU within 10 years at a speed of 14 AU/year (about 70 km/s) and function up to 400+ AU.[1] A critical technology for the mission is a large 1 g/m2 solar sail.[1] Шаблон:Pquote

In the following years there were additional studies, including the Innovative Interstellar Explorer (published 2003), which focused on a design using RTGs powering an ion engine rather than a solar sail. Another project in this field for advanced spaceflight during this period was the Breakthrough Propulsion Physics Program which ran from 1996 through 2002.

Later examples of solar sail-propelled spacecraft include IKAROS, Nanosail-D2, and LightSail.[4] Near-Earth Asteroid Scout is a planned light sail-propelled mission.[5] For comparison, the LightSail spacecraft uses a sail 5 micron in thickness, whereas they predict a sail with 1 micron thickness would be needed for interstellar travel.[3]

Other design features

The probe would use an advanced radioisotope thermoelectric generator (RTG) for electrical power, Ka band radio for communication with Earth, a Delta 2 rocket for Earth launch, and a 25 kg instrument package using 20 watts.[1]

Objectives

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Historical view of region

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See also

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References

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External links