Aperfect dresser Hot Dry Dry Hot Wet Cold Cold Wet

 


5280 the feet in a mile facto into 12 the inch in foot or 24 the hour in day this way



Moon Fact Sheet


Moon


Moon/Earth Comparison


Bulk parameters

  
   Moon   
 
   Earth   
Ratio
(Moon/Earth)
Mass (1024 kg)0.073465.97240.0123
Volume (1010 km3)2.1968108.3210.0203
Equatorial radius (km)1738.16378.10.2725
Polar radius (km)1736.06356.80.2731
Volumetric mean radius (km)1737.46371.00.2727
Ellipticity (Flattening)0.00120.003350.36
Mean density (kg/m3)334455140.606
Surface gravity (m/s2)1.629.800.165
Surface acceleration (m/s2)1.629.780.166
Escape velocity (km/s)2.3811.20.213
GM (x 106 km3/s2)0.004900.398600.0123
Bond albedo0.110.3060.360
Geometric albedo0.120.4340.28
V-band magnitude V(1,0)-0.08-3.99-
Solar irradiance (W/m2)1361.01361.01.000
Black-body temperature (K)270.4254.01.065
Topographic range (km)13200.650
Moment of inertia (I/MR2)0.3940.33081.191
J2 (x 10-6)202.71082.630.187

Orbital parameters (for orbit about the Earth)

  
   Moon   
Semimajor axis (106 km)0.3844
Perigee (106 km)*0.3633
Apogee (106 km)*0.4055
Revolution period (days)27.3217
Synodic period (days)29.53
Mean orbital velocity (km/s)1.022
Max. orbital velocity (km/s)1.082
Min. orbital velocity (km/s)0.970
Inclination to ecliptic (deg)5.145
Inclination to Earth equator (deg)18.28 - 28.58
Orbit eccentricity0.0549
Sidereal rotation period (hrs)655.720
Obliquity to orbit (deg)6.68
Recession rate from Earth (cm/yr)3.8
Mean values at opposition from Earth
        Distance from Earth (equator, km)   378,000    
        Apparent diameter (seconds of arc)     1896
        Apparent visual magnitude               -12.74     

* These represent mean apogee and perigee for the lunar orbit, 
and were used for calculating the maximum and minimum velocities.  
The orbit changes over the course of the year so the distance 
from the Moon to Earth roughly ranges from 357,000 km to 407,000 km,  
giving velocities ranging from 1.100 to 0.966 km/s. 

Lunar Atmosphere

Diurnal temperature range (equator): 95 K to 390 K  (~ -290 F to +240 F)
Total mass of atmosphere:  ~25,000 kg
Surface pressure (night): 3 x 10-15 bar  (2 x 10-12 torr)
Abundance at surface: 2 x 105 particles/cm3

Estimated Composition (night, particles per cubic cm):
    Helium 4 (4He) - 40,000 ; Neon 20 (20Ne) - 40,000 ; Hydrogen (H2) - 35,000
    Argon 40 (40Ar) - 30,000 ; Neon 22 (22Ne) - 5,000 ; Argon 36 (36Ar) - 2,000 
    Methane - 1000 ; Ammonia - 1000 ; Carbon Dioxide (CO2) - 1000 
    Trace Oxygen (O+), Aluminum (Al+), Silicon (Si+) 
    Possible Phosphorus (P+), Sodium (Na+), Magnesium (Mg+)

Composition of the tenuous lunar atmosphere is poorly known and variable, 
these are estimates of the upper limits of the nighttime ambient atmosphere 
composition.  Daytime levels were difficult to measure due to heating and 
outgassing of Apollo surface experiments.

For information on the Earth, see the Earth Fact Sheet.


The angular speed of Earth's rotation in inertial space is (7.2921150 ± 0.0000001)×10−5 radians per SI second.[36][n 4]

 Multiplying by (180°/π radians) × (86,400 seconds/day) yields 360.9856 °/day, indicating that Earth rotates more than 360° relative to the fixed stars in one solar day. Earth's movement along its nearly circular orbit while it is rotating once around its axis requires that Earth rotate slightly more than once relative to the fixed stars before the mean Sun can pass overhead again, even though it rotates only once (360°) relative to the mean Sun.[n 5] Multiplying the value in rad/s by Earth's equatorial radius of 6,378,137 m (WGS84 ellipsoid) (factors of 2π radians needed by both cancel) yields an equatorial speed of 465.10 metres per second (1,674.4 km/h).[41] Some sources state that Earth's equatorial speed is slightly less, or 1,669.8 km/h.[42] This is obtained by dividing Earth's equatorial circumference by 24 hours. However, the use of the solar day is incorrect; it must be the sidereal day, so the corresponding time unit must be a sidereal hour. This is confirmed by multiplying by the number of sidereal days in one mean solar day, 1.002 737 909 350 795,[36] which yields the equatorial speed in mean solar hours given above of 1,674.4 km/h.

The tangential speed of Earth's rotation at a point on Earth can be approximated by multiplying the speed at the equator by the cosine of the latitude.[43] For example, the Kennedy Space Center is located at latitude 28.59° N, which yields a speed of: cos(28.59°) × 1674.4 km/h = 1470.2 km/h. Latitude is a placement consideration for spaceports.




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