Документ взят из кэша поисковой машины. Адрес
оригинального документа
: http://www.iki.rssi.ru/magbase/REFMAN/EAMAGSPH/wtriad.html
Дата изменения: Unknown Дата индексирования: Fri Dec 21 21:55:24 2007 Кодировка: Поисковые слова: п п п п п п п п п п |
Triad, launched September 2, 1972, was an experimental spacecraft designed to
move in an accurately predictable low-altitude orbit, allowing its position to
be used as a reference point in navigation.
|
The Triad Spacraft.
| If the orbit were entirely determined by the Earth's gravity, it would be
easy to calculate and predict. At low altitudes, however, the air resistance
from the fringes of the atmosphere is not entirely negligible, and neither it
nor the effect of sunlight pressure can be accurately predicted. Triad had
floating inside it a "proof mass," a gold-platinum sphere about an inch across,
which, being completely enclosed, was affected neither by air resistance nor by sunlight. Even the feeble gravitational attraction of the
rest of the satellite was taken into account, by moving the power supply, radio
etc. (including the magnetometer) to the ends of two long booms, on opposite sides of the "proof mass".
|
While the "proof mass" thus moved in an accurately predictable orbit, the
spacecraft itself was subject to air resistance and sunlight pressure, causing
it to move slightly differently. Electronic sensors would note when the
floating ball approached one of the walls of its "cage", and thrustors would be
fired to move the spacecraft away from the ball. By thus matching its motion to
that of the "proof mass", the satellite moved as if the extra disturbing forces
did not exist. It worked until the spacecraft ran out of fuel. However, it was tracked for many years afterwards because of the value of its magnetometer observations.
|
"Exploration" home page (index) Glossary
Official GSFC Home Page ......... NASA WWW Home Page
Last updated March 13, 1999