Unit 2 Flashcards

1
Q

Aspiration to fly:

A

Leonardo Da Vinci (15th century): Flying machines

Kepler (17th century): Somnium; science fiction exploring soace travel

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2
Q

First Ballon with people

A

In Gondola

1783

Developed by Joseph-Michel and Jacques-Etienne Montgolfie

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3
Q

First Rockets

A

10th-century China, known as fire arrows

Gunpowder propelled

used in warfare

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4
Q

Conard Haas

A

Mid-16th Century Rockets

variety of rocket techniques even multistage rocket systems and liquid fuels

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5
Q

Willam Moore

A

was the first person to use Newton’s 3rd law to better explain rocket dynamics and propulsion in 1813

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6
Q

Willam Leitch

A

Proposed using rockets to achive spaceflight in 1861

before this rockets were military concern

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7
Q

Julies Gabriel Verne

A

significant influence on people’s thinking about spaceflight

19th Century

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8
Q

Herbert George Wells

A

19th-20th Century

Fueled public interest in the possibilities of space exploration

“Shakespeare of Science Fiction”

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9
Q

Founders of modern rocketry

A

Konstantin Tsiolkovsky (Russian)

Quian Xuesen (Chinese)

Hermann Oberth (German)
Fritz von Opel (German)
Wernhger Von Braun (German)

Robert H. Goddard (American)

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10
Q

Konstantin Tsiolkovsky:

A

Father of spaceflight

Propsed Space elevator

Rocket Equation in 1897

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11
Q

Rocket Equation

A

1897

Delta-v = change in the rocket speed
V e = exhaust velocity
M 0, m f = initial and, final masses of the rocket

bigger m 0 = bigger delta v

used to design rockets capable of reaching specific velocities required for space travel, considering factors like payload mass, fuel efficiency, and the gravitational forces they need to overcome.

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12
Q

Mass Ratio

A

m 0 / m f

The higher the mass ratio, the better

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13
Q

Mass Fraction

A

m f/ m 0

The smaller the mass fraction the better

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14
Q

Rocket Thrust (Force)

A

A rocket thrust occurs when we consume fuel faster

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15
Q

Staging

A

Allows us to discard unnecessary mass this is not needed for the rest of the flight into orbit

It is more efficient as it carries less mass, and does not start at a speed of 0

Serial: Stage 1, stage 2, …

parallel: Like serial staging But with additional strap-on rocket boosters

Hot: The first stage hasn’t finished when 2nd stage starts

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16
Q

Anatomy of a rocket

A

The fule/propellant:
The major component (most of the rocket mass)

Generates thrust and allows the rocket to move

The Rocket Body:
Structure to hold everything

The Payload:
Satellites or people

we want to minimize rocket structure mass and maximize the payload mass

The mass ratio should be as large as possible for the maximum payload

17
Q

Staging

A

allows us to discard unnecessary mass (rocket structure) that is not needed for a flight into orbit

It’s carrying less mass, and it’s not starting at a speed of 0, so it’s way more efficient

Serial: Stage 1, stage 2, …

Parallel: Like serial staging But with additional strap-on rocket boosters
They can discharge during other stages

Hot: The first stage hasn’t finished when 2nd stage starts

18
Q

Wright Brothers

A

First to fly in the atmosphere

1903

19
Q

Robert Esnauly-Pelterie

A

Independently published rocket equation

Experimented with rocket propulsion in 1931

20
Q

Rober Hutchings Goddard

A

over 200 patents

The first solid fuel (powder) rocket was launched in 1915

Liquid-fueled rockets using gasoline in 1921

His work was criticized by new york times

21
Q

Hermman Oberth

A

Rocket Car

helped work on the V2 in 1941

Joined NASA after World War 2

22
Q

Wenher Von Braun

A

Developed the V2 rocket:
Used to bomb London

started modern rocketry

Developed Saturn V:
The multistage rocket that took humanity to the moon in 1969

most powerful rocket ever built until Falcon heavy and space launch system

23
Q

Rocket Development 1950s

A

V2 was used to take photos of Earth from the atmosphere

The rockets were getting better

leading to Jupiter c then Juno 1

Juno rocket carrying Explorer 1 into orbit in Jan 1958

24
Q

Theodore von Karman

A

space starts ~100 km above mean sea level (Name Karaman Line)

Aerodynanamics stop and astronautics starts

25
Q

Lift Equation

A

L = 1/2 p v^2 S C * L

Lift >= weight for horizontal flight
L = lift force
P = air density
V = aircraft speed
S = aircraft wing area
C>L = lift coefficient

26
Q

Lift versus orbital motion

A

with increasing altitude, atmospheric air density decreases

after a point aircraft has no more lift capacity

at this altitude it’s not aerodynamics but rather astronautics

27
Q

Free Molecular Flow

A

When atmospheric density is sufficiently low molecules essentially travel in straight lines with minimal to no collision

~75-80 km above sea level

28
Q

Where are you an astronaut

A

FAI at 100km

FAA and US army 80km

29
Q

Astronaut

A

“Star sailor”

human traveling space

Astronauts (US, ESA) cosmonauts (Russia), Taikonauts (China)

30
Q

Geostationary orbit

A

appears stationary above the head

orbital inclination is 0 (above earth’s equator)

Known officially as Clarke Orbit

The higher the orbit the longer time taken to complete a revolution around the earth

31
Q

Geosynchronous orbit

A

Low inclination orbit about Earth

23 hours 56 min 4 seconds to orbit Earth

Moves with respect to an observer on the surface of the earth