Basic spacecraft concepts Flashcards

1
Q

Definition of spacecraft

A

Vehicle or machines designed to fly in outerspace

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2
Q

Definition of sub-orbital

A

enters space and then returns to the surface of the Earth - without going into permanent orbit

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3
Q

Definition of orbital

A

enters closed orbit (permanent) around Earth or other celestial body (moon)

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4
Q

Definition of interplanetary

A

travel between planets

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5
Q

Definition of interstallar

A

leave solar system

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6
Q

At what point is it considered spaceflight

A

Consider L = 0.5pSV^2Cl
as altitude increase, p decreases, therefore speed increases
when this speed = orbital speed the object stays in orbit which is considered spaceflight

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7
Q

What distance from Earth is considered space flight and what is this boundary called

A

100km above the surface

called the Karman line

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8
Q

Name the key stages of a complete space mission

A
  • Pre-launch phase
  • Launch phase
  • Orbit transfer
  • On-station operations
  • Decommisioning
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9
Q

What happens during pre-launch phase

A

ignition, separation from ground launch facilities

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10
Q

What happens during launch phase

A

placing spacecraft into an intermediate orbit

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11
Q

What happens during orbit transfer

A

transferring the spacecraft to its operational orbit

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12
Q

What happens during on-station operations

A

mission itself, station keeping, attitude control

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13
Q

What happens during decommisiong

A

place spacecraft into a higher orbit or controlled re-entry

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14
Q

What is a launch window and how long is it

A

the limited time interval available for a launch.

Typically few minutes each day. However gets much smaller when trying to rendezvous with ISS or reach another planet

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15
Q

What is Low Earth Orbit (LEO)

A
  • Altitude is 160-2000km
  • orbit period about 88-127 minutes
  • spacecraft moves with respect to Earth’s surface
  • simplest and cheapest, high bandwidth and low communication delay
  • see Earth’s surface more clearly
  • most statellites and ISS are in LEO
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16
Q

What is Geostationary Earth Orbit (GEO)

A
  • Altitude is 35,786km above equator
  • Orbital period is 24hrs, therefore at a fixed position with respect to Earth’s surface
  • used for communication and weather satellites
  • high cost, communication delay of 0.25seconds
17
Q

How do chemical rockets change momentum

A

by discharging hot products of combustion at very high velocities
high power but limited energy

18
Q

How does electrical propulsion work and why is it useful

A

by electrically heating or charging particals to increase kinetic energy
useful as it is not energy limited and so used for station keeping and interplanetary missions

19
Q

Rocket equation

A

ΔV = Vex . ln(Mo/M1)

where:
ΔV = change in velocity
Vex = exhaust velocity
Mo = initial mass of rocket inc. fuel
M1 = final mass after fuel burn
20
Q

Calculating mass of the propellant (fuel)

A

Mprop = Mo - M1

Mprop = Mo(1 - e^-(ΔV/Vex))