To determine the overall reliability of the solar instrument, we can calculate the probability of all components functioning simultaneously. The overall reliability is the product of the individual reliabilities: ( 0.92 \times 0.87 \times 0.64 \approx 0.514 ). Therefore, the instrument has an overall reliability of about 51.4%, meaning that there is a 48.6% chance that at least one component will fail and the instrument will not function.
To build a satellite, you need to first define its purpose and specifications. Then, design the satellite components, such as structure, power systems, communication systems, and payloads. Finally, assemble the components, test the satellite thoroughly, and launch it into orbit.
an instrument called a satellite
A satellite.
SATELLITE
Leda & Lysithea, the 10th and 12th of Jupiter, respectively.
revolutionary advances in jet aircraft, missile technology, satellite systems, digital computers, miniaturization of electronic components, and the specialized needs of the space program
The power of the engine and the maximum speed of the 1971 Plymouth Satellite is 425 hp (317 kW) and 150 mph respectively.
A negative impact on a satellite could be damage caused by space debris colliding with the satellite, which can result in malfunctions or complete loss of the satellite. Additionally, exposure to high levels of radiation in space can degrade the satellite's components over time, affecting its performance.
One would be best going to the organisation called ehow to find more detailed information about satellite components. It is an independent organisation that offers help and does not try to sell.
In general the farthest point in a satellite's orbit from its focus is its apoapsis. If the focus is the Sun or Earth however then you would say the satellite's farthest point is its aphelion and apogee, respectively.
Landsat satellite
When it is closest to the planet.One of the components of the acceleration, the normal acceleration, is equal to v2/r, where v is the satellite's speed and r is the radius of the current orbit followed by the satellite. So, the smaller the radius, the higher the acceleration.