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The Space Elevator

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Time-to-Double (TD) We cam only launch (by rockets) fraction-sized ... Characteristic Time Constant. The time it takes the Space Elevator to lift its own weight ... – PowerPoint PPT presentation

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Title: The Space Elevator


1
TheSpaceElevator
  • A Space Odyssey

Ben Shelef ben_at_spaceward.org http//www.space
ward.org
2
2009 Games at NASA Dryden
Official Trailer
3
TheSpaceElevator
  • A Space Odyssey

Ben Shelef ben_at_spaceward.org
4
1960 ? ? ?
5
The Early Days
USA First Satellite 1958 Man in Orbit 1962
USSR First Satellite 1957 Man in Orbit 1961
6
Space Fever
7
Yuri Artsutanov
To the Cosmosby Electric Train
Tsiolkovskysrocket equation
8
The trouble with rockets
9
Drop a cable from a satellite
Counter-weight
24 hrs.
Very long cable
Too slow (30 days) 240,000 miles
Just right (GEO) 25,000 miles
Too low (LEO) 150-500 miles overhead 90 minutes
24 hrs.
10
Swing a ball on a string
1 foot string ? 1.1 seconds (or less) to go
around
1500 foot string ? 42 seconds (or less) to go
around
86,400 seconds (one day) to go around ? String
needs to be at least 25,000 miles long
11
The 25,000 mile problem
How long can a cable be before it breaks under
its own weight?
Steel wire get usabout 50 miles
Advanced Kevlar and similar materials get us a
bit more than 250 miles
Until recently, no known material even come close
to what we need for a Space Elevator
12
The power problem
  • During the beginning of the trip, 20 ton climber
    ascending at 50 m/s is drawing 10 MWatt of power.
  • How do we power a climber?
  • Will the mass of the power system exceed the mass
    of the climber?
  • Where do we store the energy?

13
??? 1990 .
14
Carbon Nanotubes
  • New class of molecules tubes of carbon atoms
  • Discovered in 1991 by Sumio Iijima
  • Individual nanotubes are 30 times stronger than
    steel and 6 times lighter
  • A tether made out of Carbon Nanotubes will
    bestrong enough to construct the Space Elevator !

15
Photonics
  • New breed of electrical lasers featuring
    acceptable efficiencies, wavelengths, and
    lifetimes.
  • Multi-MWatt systems are feasible.
  • New breed of very light thin-film PV cells.
  • Power densities of several kWatt/kg are feasible.
  • With power beaming, leave the power system!
  • Safe, Reliable, Low Cost.

16
The Modern Space Elevator
  • A space launch system that can carry tons per
    day, to any destination in the Solar System, at
    extremely low costs.
  • No smoke, no fire safe and environmentally
    friendly.
  • No stress travel at a leisurely 120 mph,
    transition gently from 1g to 0g.
  • Infinitely scalable there is no limit onhow
    large (or small)a Space Elevatorcan be.

17
or travel to the end of the ribbon and get
slung to an Earth escape trajectory no extra
fuel necessary!
Step off into orbit at GEO
  • Destinations
  • LEO, GEO
  • Moon, Mars
  • Venus, Asteroids

24 hrs.
18
Our Sponsors
Thank you!
(Your Company Name Here)
19
Movie Time v.1
20
Movie Time v.2
21
The Bad News
  • First estimates placed CNTs at 100 N/Tex
  • Recent estimates are in the 40 50 N/Tex range
  • How strong does the tether really have to be?
  • Is this a show-stopper?

(Stone-Wales Defect Formation)
22
The Good News
  • 400 m2 total area
  • 32 kg including structure and deployment
    mechanism (at center)
  • 50 kWatt (lt10 efficient)
  • 1.5 kWatt/kg today, potential for 3-5 kWatt/kg

23
Eat Your Cake and Have it Too !
  • If the tether is weaker/heavier than expected
  • The taper ratio will increase
  • The ratio of tether mass to payload capacity
    (TMR) will increase
  • Not fatal railroads are always heavier than the
    trains!
  • If the power system is weaker/heavier than
    expected
  • Well move slower
  • Well carry less payload
  • Our Payload Mass Throughput (PMT) is reduced
  • Still much better than rockets!
  • Really?

24
The Space Elevator Feasibility Condition
  • Tether lifetime (TL)
  • Every material degrades UV, Micrometeorites
  • Entire tether must be replaced every TL years
  • Time-to-Double (TD)
  • We cam only launch (by rockets) fraction-sized
    Space Elevators
  • Orbital spares are fraction size (FS)
  • Characteristic Time Constant
  • The time it takes the Space Elevator to lift its
    own weight

25
The Space Elevator Feasibility Condition
  • Assuming, TD 1.5 years, FS 25, TL 6 years
  • ? CTC 1 yr.
  • Impossible lt Space Elevators lt Easy

26
So Back to the Games!
  • July 14, NASA Dryden Flight Research Center,
    Mojave, CA
  • 6 teams, up to 2,000,000 in prize purse
  • Looking for additional sponsorships!

27
Our Sponsors
Thank you!
(Your Company Name Here)
28
Contact
  • http//www.elevator2010.org
  • http//www.spaceward.org
  • ben_at_spaceward.org
  • 650-793-4987
  • 725 N Shoreline Blvd.
  • Mountain View, CA 94043

29
FIN
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