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C. Hall, Randolph 224D [email protected] AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles Space law and policy Space industry Daily Quizzes Final Exam (Comprehensive)

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Page 1: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

AOE 2104 - The Space Part• Introduction to space systems

concepts• Space environment• Orbital mechanics• Launch vehicles• Space law and policy• Space industry• Daily Quizzes• Final Exam (Comprehensive)

• Introduction to space systems concepts

• Space environment• Orbital mechanics• Launch vehicles• Space law and policy• Space industry• Daily Quizzes• Final Exam (Comprehensive)

Page 2: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

ReadingDava Newman, Interactive

Aerospace Engineering and Design, McGraw-Hill, 2002

• Background: Sections 1.7 – 1.10, Chapter 2

• Space Environment: Chapter 8• Orbital Mechanics: Chapter 9• Satellite Systems Engineering:

Chapter 10• Human Space Exploration: Chapter

11

Dava Newman, Interactive Aerospace Engineering and Design, McGraw-Hill, 2002

• Background: Sections 1.7 – 1.10, Chapter 2

• Space Environment: Chapter 8• Orbital Mechanics: Chapter 9• Satellite Systems Engineering:

Chapter 10• Human Space Exploration: Chapter

11

Page 3: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Sample Space Applications

Communications Navigation RelayWeather Surveillance ScienceMaterials processing Search &

rescueAstronomy Weapons

TourismSpace Exploration Solar PowerTransportation Colonization

Mapping

Communications Navigation RelayWeather Surveillance ScienceMaterials processing Search &

rescueAstronomy Weapons

TourismSpace Exploration Solar PowerTransportation Colonization

Mapping

Page 4: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Basic Elements of Space Missions

• Subject - the “thing” which interacts with or is sensed by the payload

• Space segment - spacecraft comprised of payload and spacecraft bus

• Launch segment - launch facilities, launch vehicle, upper stage. Constrains spacecraft size.

• Orbit/constellation - spacecraft’s trajectory or path through space

• C3 Architecture - command, control and communications

• Ground segment - fixed and mobile ground stations necessary for TT&C

• Mission operations - the people, policies and procedures occupying the ground (and possibly space) segments

• Subject - the “thing” which interacts with or is sensed by the payload

• Space segment - spacecraft comprised of payload and spacecraft bus

• Launch segment - launch facilities, launch vehicle, upper stage. Constrains spacecraft size.

• Orbit/constellation - spacecraft’s trajectory or path through space

• C3 Architecture - command, control and communications

• Ground segment - fixed and mobile ground stations necessary for TT&C

• Mission operations - the people, policies and procedures occupying the ground (and possibly space) segments

Page 5: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Space segment

Payload

Bus

Ground Segment

MissionOperations

LaunchSegment

Orbit andConstellation

Subject

Command, Control andCommunications

Architecture

Reference: Larson & Wertz, Space Mission Analysis and Design

Reference: Larson & Wertz, Space Mission Analysis and Design

Page 6: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Payload and Bus Subsystems

S e n so rsC a m e rasA n te nn as

R a d ar

Payload

Pow erS o la r a rra ys

B a tte riesP M A D

ADC SS e n so rs

A c tua to rsP ro ce sso rs

Therm al ControlC o atin gsIn su la tion

A c tive co n tro l

TT& CP o w e r sw itch ingE n cod e r/d e co d er

P ro ce sso rs

PropulsionO rb it in je c tion

S ta tio nke ep ingA tt itu d e co n tro l

StructureP rim a ry s tru c tu re

D e p loym e ntm e ch an ism s

Bus

Spacecraft

Basic requirements• Payload must be

pointed• Payload must be

operable• Data must be

transmitted to users

• Orbit must be maintained

• Payload must be “held together”

• Energy must be provided

Basic requirements• Payload must be

pointed• Payload must be

operable• Data must be

transmitted to users

• Orbit must be maintained

• Payload must be “held together”

• Energy must be provided

Page 7: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Thoughts on SpaceSome comments overhead at the Officer’s Club

• It’s a really big place with no air.

• There’s nothing out there, is there?

• How many g’s is that satellite pullingwhen the ground track makes those turns?

• Why can’t I have my spy satellitepermanently positioned over Moscow?

• It’s a really big place with no air.

• There’s nothing out there, is there?

• How many g’s is that satellite pullingwhen the ground track makes those turns?

• Why can’t I have my spy satellitepermanently positioned over Moscow?

Page 8: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Useful Characteristics of Space

• Global perspective or “There’s nothin’ there to block your view”

• Above the atmosphere or “There’s no air to mess up your view”

• Gravity-free environment or “In free-fall, you don’t notice the gravity”

• Abundant resources or “Eventually, we will mine the asteroids, collect more solar power, colonize the moon, . . .”

• Global perspective or “There’s nothin’ there to block your view”

• Above the atmosphere or “There’s no air to mess up your view”

• Gravity-free environment or “In free-fall, you don’t notice the gravity”

• Abundant resources or “Eventually, we will mine the asteroids, collect more solar power, colonize the moon, . . .”

Page 9: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Global Perspective

Amount of Earth that can be seen by a satellite is much greater than can be seen by an Earth-bound observer.

Low-Earth orbit is closer than you think.

Amount of Earth that can be seen by a satellite is much greater than can be seen by an Earth-bound observer.

Low-Earth orbit is closer than you think.Space isn't remote at all. It's only an hour's drive away if your car could go straight upwards.

— Fred Hoyle

Page 10: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Instantaneous Access Area

Example: Space shuttleExample: Space shuttle

HR

R

K

KIAA

e

e

A

A

cos

km 1055604187.2

)cos1(28

2km 628,476,11

24.179551.0cos

km 300H

km 6378

IAA

Re

Re

H

A friend of mine once sent me a post card with a picture of the entire planet Earth taken from space. On the back it said, “Wish you were here.”

— Steven Wright

IAA

Page 11: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Above the Atmosphere

• This characteristic has several applications Improved astronomical observations“Vacuum” for manufacturing processesLittle or no drag to affect vehicle motion

• However, there really is “air” in space Ionosphere affects communications signals“Pressure” can contaminate some

processesDrag causes satellites to speed up (!) and

orbits to decay, affecting lifetime of LEO satellites

• This characteristic has several applications Improved astronomical observations“Vacuum” for manufacturing processesLittle or no drag to affect vehicle motion

• However, there really is “air” in space Ionosphere affects communications signals“Pressure” can contaminate some

processesDrag causes satellites to speed up (!) and

orbits to decay, affecting lifetime of LEO satellites

Page 12: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Vacuum Effects• While space is not a perfect vacuum, it is

better than Earth-based facilities200 km altitude: pressure = 10-7 torr = 10-5 PaGoddard vacuum chambers: pressure = 10-7

torr

• Outgassingaffects structural

characteristicspossibility of

vapor condensation

• While space is not a perfect vacuum, it is better than Earth-based facilities200 km altitude: pressure = 10-7 torr = 10-5 PaGoddard vacuum chambers: pressure = 10-7

torr

• Outgassingaffects structural

characteristicspossibility of

vapor condensation

Wake Shield Facility (shuttle experiment)

Page 13: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Atmospheric Drag• Can be modeled same as with “normal” atmospheric

flight

• Key parameter is the “ballistic coefficient”:

• Larger ballistic coefficient (small massive satellite) implies slower orbital decay

• Smaller ballistic coefficient implies faster orbital decay • Energy loss per orbit is

• Can be modeled same as with “normal” atmospheric flight

• Key parameter is the “ballistic coefficient”:

• Larger ballistic coefficient (small massive satellite) implies slower orbital decay

• Smaller ballistic coefficient implies faster orbital decay • Energy loss per orbit is

HhSL

D

e

VACD/

221

)/( ACm D

rD2

Better not take a dog on the space shuttle, because if he sticks his head out when you're coming home his face might burn up. — Jack Handey

Page 14: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

WeightlessnessThis illustration from Jules Verne’s Round the Moon shows the effects of “weightlessness” on the passengers of The Gun Club’s “bullet” capsule that was fired from a large gun in Florida.

The passengers only experienced this at the half-way point between the Earth and the Moon.Physically accurate?

This illustration from Jules Verne’s Round the Moon shows the effects of “weightlessness” on the passengers of The Gun Club’s “bullet” capsule that was fired from a large gun in Florida.

The passengers only experienced this at the half-way point between the Earth and the Moon.Physically accurate?

Page 15: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Zero-Gravity?

This plot shows how gravity drops off as altitude increases.Note that at LEO, the gravitational acceleration is about 90% of that at Earth’s surface.

This plot shows how gravity drops off as altitude increases.Note that at LEO, the gravitational acceleration is about 90% of that at Earth’s surface.

Page 16: C. Hall, Randolph 224D cdhall@vt.edu AOE 2104 - The Space Part Introduction to space systems concepts Space environment Orbital mechanics Launch vehicles

C. Hall, Randolph [email protected]

Microgravity• Weightlessness, free fall, or zero-g

• Particles don’t settle out of solution, bubbles don’t rise, convection doesn’t occur

• Microgravity effects in LEO can be reduced to 10-1 g (1 g)

• Weightlessness, free fall, or zero-g

• Particles don’t settle out of solution, bubbles don’t rise, convection doesn’t occur

• Microgravity effects in LEO can be reduced to 10-1 g (1 g)

On Earth, gravity-driven buoyant convection causes a candle flame to be teardrop-shaped (a) and carries soot to the flame's tip, making it yellow. In microgravity, where convective flows are absent, the flame is spherical, soot-free, and blue (b).