htv edt propulsion conceptual studyriemann.math.wichita.edu/media/physicsseminar2015/... ·...
TRANSCRIPT
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CONVENTIONAL ROCKET
PROPULSION
NON-CONVENTIONAL PROPULSION
SOLAR SAILS
TETHERS
ELECTRIC SAILS
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THE REASON?
DISTANCE!!!
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CONVENTIONAL ROCKET
PROPULSION
NON-CONVENTIONAL PROPULSION
SOLAR SAILS
TETHERS
ELECTRIC SAILS
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A motional electromotive force is generated across a
tether as it moves relative to the Earth’s magnetic field
given by Faraday’s Law of Induction
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A motional electromotive force is generated across a
tether as it moves relative to the Earth’s magnetic field
given by Faraday’s Law of Induction
The tether moves relative to the Earth’s magnetic field. The positive
end of the tether collects ionospheric electrons forming an electrical
current; a force on the wire will be generated via the Lorentz Force
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Magnetic field strength
and direction varies over
each orbit
Forces have components
both:
In-plane (orbit
raising/lowering)
Out-of-plane
(inclination change)
Tether current can be
modulated over one or
more orbits to change all
six orbital elements
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spacecraft launch datelaunch
vehicleorbit mass
SEDS 1 +
deployerMar. 30, 1993 Delta 7925
195 × 705 ×
34°25 kg
SEDS 2 +
deployerMar. 10, 1994 Delta 7925
350 km
(circular)25 kg
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Jovian Electrodynamic Capture
Hyperbolic Intercept
Electrodynamic
Decay Region
(V in km/sec)
0.03
0.06
0.12
0.33
0.73Perijove = 1.2 RJ
Parabolic 100 Day
Capture Orbit
(0.5 km/sec V
required for capture)
V= 5 km/sec
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Tethered Satellite System
before it broke
Tethered Satellite System after it
separated from the Space Shuttle
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CONVENTIONAL ROCKET
PROPULSION
NON-CONVENTIONAL PROPULSION
SOLAR SAILS
TETHERS
ELECTRIC SAILS
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Sail
Thrust
Vector
Sun
Angle
Incident
Photons
Reflected Photons
Sail
“normal
vector”
Sail
Thrust
Vector
Sun
Angle
Incident
Photons
Reflected Photons
Sail
normal
vector
Real Solar Sails Are Not “Ideal”
Sail
Thrust Vector
Sun
Angle
Incident
Photons
Reflected Photons
Sail
normal
vector
Ideal Case
Billowed QuadrantDiffuse Reflection
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Thrust Vector Components
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SailF(normal)
Sun Angle
Reflected Photons
Sail normal
vector
CM
CP
F(tangential)
F(total)
M(total)
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Image courtesy of Colorado Center for Astrodynamics Research
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• 135-foot rigidized inflatable balloon satellite • laminated Mylar plastic and aluminum • placed in near-polar Orbit • passive communications experiment by NASA on January 25, 1964
When folded, satellite was packed into the 41-inch diameter canister shown in the foreground.
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Znamya (Space Mirror)
♦ Russian experiment that flew
on Progress after undocking
from Mir Space Station in
1993.
♦ Purpose was to reflect sunlight
onto the ground from space.
♦ 20-m diameter sail
successfully deployed
♦ 5-km spot illuminated Europe
from France to Russia moving
at 8 km/sec.
♦ Follow-on mission flew, but
was damaged during
deployment.
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NASA GROUND TESTED SOLAR SAILS IN THE MID-2000’S
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♦ Two solar sail technologies were designed, fabricated, and tested under thermal vacuum conditions in 2005:
♦ Developed and tested high-fidelity computational models, tools, and diagnostics
♦ Multiple efforts completed: materials evaluation, optical properties, long-term environmental effects, charging issues, and assessment of smart adaptive structures
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400 m2
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NANOSAIL-D DEMONSTRATION SOLAR SAIL
♦ 10 M2 SAIL
♦ MADE FROM TESTED GROUND DEMONSTRATOR HARDWARE
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NanoSail-D in Flight
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Interplanetary Kite-craft Accelerated by Radiation
of the Sun (IKAROS)
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Interplanetary Kite-craft Accelerated by Radiation
of the Sun (IKAROS)
Jacob Peter Gowy's
The Flight of Icarus
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5 to 100 m DIA
= 10 g/m2
500 - 800-m DIA
= 1 - 2.5 g/m2
MID-TERM
SAILS
2015 - 2025
4000-m DIA
0.1 g/m2
1-km DIA
= 0.1 g/m2
INTERSTELLAR PROBE
2025 - 2050
• NEA Scout / Lunar Flashlight
• Solar Polar Imager
• NON-KEPLERIAN EARTH ORBITS
TECH
DEV
TECH
DEV
TECH
DEV
TECH
DEV
TECH
DEV
INTERSTELLAR
MEDIUM EXPLORATION
• NanoSail-D
• LightSail
• InflateSail/CubeSail
= Areal Density (Sail Mass/Sail
Area)
4.5 LY
INTERSTELLAR
PROBE FLYBY
40 LY
INTERSTELLAR
PROBE
RENDEZVOUS
• INTERSTELLAR PROBE
• EUROPA LANDERS
• COMET SAMPLE RETURN
• OORT CLOUD
4-km DIA
= 0.1 g/m2
1000-km DIA
= 0.1 g/m2
NEAR-TERM
SAILS
2010 - 2015
3 – 5 m DIA
Solar Powered
Laser Powered
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CONVENTIONAL ROCKET
PROPULSION
NON-CONVENTIONAL PROPULSION
SOLAR SAILS
TETHERS
ELECTRIC SAILS
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•
•
Electric Sail Concept
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