OEM 101 Flashcards

1
Q

What kind of Orbits are the most commonly used orbital regime?

A

LEO Orbits

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2
Q

What is the period and altitude of LEO?

Period: time it takes for one orbit

A

A period of 90 to 120 minutes and an altitude of < 2000 km

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3
Q

What does LEO stand for?

A

Low earth orbit

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4
Q

What type of missions are LEO orbits involved with?

A

SATCOM: iridium and star link
Earth observation
Weather/earth sensing/ISR

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5
Q

What does MEO stand for?

A

Medium earth orbit

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6
Q

MEO has a period of what?

A

Milo has a period of greater than 120 minutes in less than 24 hours.

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7
Q

What missions does MEO support?

A

Position, navigation, timing (PNT)
SATCOM
Persistent earth, observation

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8
Q

What is the period of a geosynchronous orbit (Geo)?

Period: time it takes for one orbit

A

24 hours, matches the rotational speed of the earth.

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9
Q

MEO orbit with a period at about 12 hours is called what?

A

Semi synchronous orbit

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10
Q

What is the altitude of Geo?

A

35,786 km

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11
Q

What missions are covered in Geo?

A

SATCOM Dash DSCS, MILSTAR, WGS
Weather – GOES
Missile warning, Dash SBIRS GEO, DSP

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12
Q

Three satellites in GEO can give ________ coverage with the exception of the polar regions.

A

Global

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13
Q

what GEO orbit has an inclination and eccentricity that both equal zero?

A

Geo-stationary orbit

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14
Q

What special orbit is it near the polar inclination, and is in Leo orbit with a retrograde motion?

A

Sun-synchronous orbit

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15
Q

What orbits primarily support the mission of SATCOM and missile warning?

A

Highly-elliptical orbits (HEO)

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16
Q

What is the field of regard?

A

It is the portion of the Earth surface that is geometrically visible from the satellites position in space.

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17
Q

What is the field of view?

A

It is the instantaneous coverage area capable of being seen by the payload.

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18
Q

The length of time a satellite has line of sight to a point on earth is called what?

A

Dwell time

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19
Q

Which orbit is highly eccentric, it’s orbit creates Longville times, covers the gap left by the GEO constellation and it is normally over northern latitudes mission requirements?

A

Highly elliptical orbit (HEO)

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20
Q

Give two examples of highly elliptical orbits (HEO)? By name.

A

Molniya orbit
Tundra orbit

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21
Q

A Satellite at a _______ altitude will be moving _______ Intend to have a shorter dwelltime.

A

Lower, faster

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22
Q

What reference frame is used to describe orbits, define classical orbital elements, and is considered non-rotating?

A

The ecliptic reference frame

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23
Q

What reference frame is used to describe ground tracks, the path, a satellite travels, relative to the Earth surface and is considered rotating with earth?

A

ECEF reference

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24
Q

What angle do we used to determine when to do a lunch, in order to launch any specific are R a a N?

A

Sidereal angles

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25
What describes were defines the size of an orbit?
Semi major axis
26
Define eccentricity.
The shape of an orbit.
27
What is the apogee?
The furthest point from the Earth.
28
What is the perigee?
The closest point to the Earth.
29
Are the inclination describes the _____ of the orbit.
Tilt
30
The inclination of a satellite orbiting earth is measured off of the ___________.
Equatorial plane
31
Eccentricity in their corresponding shapes.
Take minute to study! E = 0 circle 0 < e < 1 ellipse e= 1 parabola e > 1 hyperbola
32
What is the corresponding shape to the eccentricity e = 0
Circle
33
What is the corresponding shape to the eccentricity e >1?
Hyperbola
34
What is the corresponding shape to the eccentricity 0 < e < 1?
Ellipse
35
What is the corresponding shape to the eccentricity e= 1?
Parabola
36
The inclination is measured from the __________ to the _________.
The inclination is measured from the equatorial plane to the orbital plane.
37
True anomaly defines the satellites ________.
Location
38
Right ascension of the sending no defines the ______ of the orbit
Twist
39
The right ascension of the sending node ( RAAN) is measured from the ________ to the _______.
Vernal equinox, ascending node
40
Types of orbits and their degrees.
Take a minute to study! i = 0°, 180° : equatorial i = 90° : polar 0° < i < 90° : prograde 90° < i < 180° : retrograde
41
Name the type of orbit : i = 0°, 180°
equatorial
42
Name the type of orbit : i = 90°
Polar
43
Name the type of orbit : 90° < i < 180°
Retrograde
44
Name the type of orbit: 0° < i < 90°
Prograde
45
The argument of perigee is measured from the _________ to __________.
Ascending node to the perigee
46
_________ describes orientation of an orbit with in the orbital plane.
Argument of perigee
47
The true anomaly describes the ______ of a satellite within the orbit.
Location
48
True anomaly is measured from the_______ to the _________ _________.
Perigee, satellite location
49
How long is the period of a satellite and Leo ?
90-120 minutes
50
Which orbits inclination eccentricity both equal 0, is it GEO-stationary or Geo-synchronous?
Geo-stationary
51
What orbit creates long do all times, normally over the northern latitudes permission requirements?
HEO or highly elliptical orbit
52
What operational consideration describes a portion of the Earth surface that is geometrically visible from the satellites position in space?
Field of regard
53
What operational consideration describes the instantaneous coverage area capable of being seen by the payload?
Field of view
54
What operation consideration describes the length of time a satellite has line of sight to a point on earth?
Dwell time
55
Semi major axis = _________ Range? Description?
=a Range : 0 to infinity Description : size of orbit
56
Eccentricity =__________ Range? Description?
= e Range : 0 to 1 Description : shape of orbit
57
Inclination = _________ Range? Description?
=i Range : 0 to 180° Description: tilt of orbit
58
(RAAN) right ascension of the descending node = ________ Range? Description?
= “omega symbol” Range : 0 to 360° Description : twist of orbit
59
Argument of perigee =_________ Range? Description?
=w Range : 0 to 360° Description : orientation of orbit
60
True anomaly = _________ Range? Description?
= v Range : 0 to 360° Description : location of orbit
61
Which of newtons laws states- to every action there is always an opposed and equal reaction?
Third law
62
Which of newtons laws states - an object either remains at rest, or continues to move at a constant velocity, unless acted upon by an external force?
First Law
63
Which of newtons laws state-any two bodies attract one another, with a Force, proportional to the product, their masses and inversely proportional to the square of the distance between them?
Law of Universal gravitation
64
Which of newtons laws states - the rate of change of momentum is proportional to the Force impressed, and is in the same direction as the force?
Second law
65
Which of Kepler’s laws states - the planets, orbit the sun in elliptical orbits, with the sun at one focus of the ellipse?
First law
66
Which of Kepler’s laws states - the period of the orbit squared is proportional to the semi major axis cubed?
Third law
67
How long is a sidereal day?
Approximately 23 hours 56 minutes in 04.09 seconds.
68
What are the three fundamental plans?
Equatorial plane, ecliptic plane, orbital plane
69
Equatorial plane
Passes through earths equator
70
Ecliptic plane
Plane of earths orbit around the sun (separated from equatorial plane due to the tilt of earths axis)
71
Which of Kepler’s laws states the orbiting body must be moving faster when it is closer and slower when it is farther away?
Second law
72
What does ECI stand for?
Earth centered inertial frame
73
And what is the principal direction of ECI?
Vernal equinox
74
What is the origin of ECI?
Earth
75
What is the fundamental plane of ECI?
Equatorial
76
What does ECEF stand for?
Earth centered earth fixed frame
77
What is the origin of ECEF?
Earth
78
What is the fundamental plane of ECEF?
Equatorial
79
What is the principal direction of (ECEF) earth centered earth fixed frame?
0° latitude, 0° longitude “rotating with the Earth”
80
Is earth centered inertial rotating or non-rotating?
Non-rotating
81
Is earth centered earth fixed rotating, or non-rotating?
Rotating
82
The ECI in the ECEF reference frames utilize what as their fundamental plan?
Equatorial plane
83
Define perifocal frame.
The perifocal frame is a frame of reference from an orbit. The frame is centered at the focus of the orbit ( the celestial body about which the orbit is centered)
84
What does RIC stand for?
Radio in track cross track frame
85
What is the origin of the perifocal plane?
Earth
86
What is the fundamental plane of the perifocal plane?
Orbital
87
What is the principal direction of the perifocal plane?
Eccentricity of vector (points towards perispsis)
88
What is the origin of RIC (radical in track cross track frame) ?
Satellite
89
What is the fundamental plane of RIC ( radical in track cross track frame) ?
Orbital
90
What is the principal direction of RIC ( radical in track cross frame) ?
Radical (points, directly way from the Earth)
91
I which reference frame uses a satellite as its origin?
( RIC) radical and track cross track
92
What is the principal direction of the perifocal reference frame?
Eccentricity vector
93
What is the principal direction of the RIC reference frame?
Radical
94
We use the sidereal angle to determine ________ to do a launch.
When
95
Sidereal time is measured as the angle between the_______ of the earths-inertial and ________ frames
principal axes, earth-fixed
96
What does SSO stand for?
Sun -synchronous orbit
97
How long is the period of a satellite and Leo?
90 to 120 minutes
98
The same sun, angle or shadow every orbit is a characteristic of what orbit?
Sun-synchronous orbit (SSO)
99