Question
In: Physics
what would the equilibrium temperature of the earth be if it were in mars's orbit? what...
what would the equilibrium temperature of the earth be if it were in mars's orbit? what about venus's orbit?
Solutions
genius_generous answered 6 months agoRelated Solutions
· Assuming no earth atmosphere, what the expected temperature of the earth would be? How this...
· Assuming no earth atmosphere, what the expected temperature
of the earth would be? How this temperature could be
estimated?
· Most notable CO2 monitoring station is at Mauna Loa
Observatory in Hawaii. Why the CO2 concentration changes with
season during the year?
· With current rate of CO2 addition to the atmosphere, assuming
this rate is constant, how long it will take to double the CO2
atmosphere concentration?
· What kinds of effect the global warming may have on...
What factors affect the speed of a satellite in circular orbit around Earth. And, how would...
What factors affect the speed of a satellite in circular orbit
around Earth. And, how would you calculate that speed?
A hollow hoop and a solid disk are released from rest at the top
of an incline plane that has friction. Which will reach the bottom
of the hill first and why?
What is impulse and how does it relate to the average force
applied to an object during a collision? Include one physical
example in your explanation.
A geostationary satellite is in a circular orbit around the Earth. What is the linear speed...
A geostationary satellite is in a circular orbit around the
Earth. What is the linear speed of the satellite?
What would be the appropriate equilibrium temperature of a system obtained by adding 25.0 g of...
What would be the appropriate equilibrium temperature of a
system obtained by adding 25.0 g of ice at 0°C to 250.0 mL of "hot"
(80°C) coffee, assuming that the heat capacity and density of the
coffee are the same as for pure water (4.18 J g-1 °C-1 and 0.997 g
mL-1), and also assuming negligible heat transfer with the
surroundings? [For water, ΔHfusion = 6.02 kJ/mol.]
*Note: the answer is 65 deg C
A 590-kg satellite is in a circular orbit about Earth at a height above Earth equal...
A 590-kg satellite is in a circular orbit about Earth at a
height above Earth equal to Earth's mean radius.
(a) Find the satellite's orbital speed.
m/s
(b) Find the period of its revolution.
h
(c) Find the gravitational force acting on it.
N
Calculate at what distance from the centre a satellite has to orbit Earth (of mass 6...
Calculate at what distance from the centre a satellite has to
orbit Earth (of mass 6 x 10 24 kg) if it period or revolution is to
equal Earth’s rotation period of 23h 56m (about 86, 160 seconds.)
What is important about such a satellite? c) The mass of the moon
is 81 times smaller (7.4074x 10 22 kg) and the period of orbit is
27.3 days. (Convert using 86, 400 sec = 1 day.) What should the
radius of...
A satellite is being designed to completely orbit the Earth 4 times per day. At what...
A
satellite is being designed to completely orbit the Earth 4 times
per day. At what velocity must this satellite have in order to keep
the orbit circular?
Take
the mass of the Earth to be
5.97×1024
kg.
A satellite is put into an elliptical orbit around the Earth. When the satellite is at...
A satellite is put into an elliptical orbit around the Earth.
When the satellite is at its perigee, its nearest point to the
Earth, its height above the ground is hp=215.0 km,hp=215.0 km, and
it is moving with a speed of vp=8.450 km/s.vp=8.450 km/s. The
gravitational constant GG equals 6.67×10−11 m3⋅kg−1⋅s−26.67×10−11
m3·kg−1·s−2 and the mass of Earth equals 5.972×1024 kg.5.972×1024
kg.
When the satellite reaches its apogee, at its farthest point
from the Earth, what is its height haha above...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at...
A satellite is put into an elliptical orbit around the Earth.
When the satellite is at its perigee, its nearest point to the
Earth, its height above the ground is ℎp=215.0 km, and it is moving
with a speed of ?p=8.850 km/s. The gravitational constant ? equals
6.67×10−11 m3·kg−1·s−2 and the mass of Earth equals 5.972×1024 kg.
When the satellite reaches its apogee, at its farthest point from
the Earth, what is its height ℎa above the ground? For this...
A satellite is placed in an elongated elliptical (not circular) orbit around the Earth. At the...
A satellite is placed in an elongated elliptical (not circular)
orbit around the Earth. At the point in its orbit where it is
closest to the Earth, it is a distance of 1.00 × 10^6
m from the surface (not the center) of the Earth,
and is moving at a velocity of 5.14 km/s. At the
point in its orbit when it is furthest from the Earth it is a
distance of 2.00×10^6 m from the surface of the
Earth....
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