Short Beamed Energy SA

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    Beamed Energy and$100/kg to GEO

    On how power in space gives rise to

    low cost transport and how to get

    started

    Keith Henson (L5 Society)

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    Simple analysis

    10 year return on capital, 80,000 hours

    $1600/kW can be paid back at 2 cents per

    kWh (Below coal to get market share) $200/kW rectenna, $900/kW parts and labor

    ($450 before transmission loss), $500/kW

    for transport to GEO At 5 kg/kW requires

    $100/kg or less to GEO

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    Cant be done with chemical fuel

    Current $20,000/kg to GEO

    SpaceX $4,000/kg $1,000/kg 20t/1400t, 1.4% payload

    Skylon ~$1000/kg

    $500/kg 7t/300t, 2.3% payload

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    40 kg, but just scaling from MW

    to GW, move to Equator, cover

    mountain with gyrotrons, run 4

    minutes out of 20, 11 milliontruck batteries, 5 years and they

    die, but in that time 500 GW of

    SBSP. Silly to send power down

    and back up so . . . .

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    4 5 6 7 8 9 10 11

    0

    10

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    Percent payload (blue)

    GW x 10 (orange)

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    Hydrogen combustion to 25 km, &

    Mach 5.5 Laser heated hydrogenabove that point (laser beamed down

    from GEO) 3.4 GW of laser

    Performance analysis, 54 t to LEO

    Vehicle 24 t, (20% structure) plus 30 t second stage to LEO

    2/3rd of second stage to GEO (20 t)

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    105 kW CW

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    Cost breakdown

    Vehicle amortization $10/kg

    Hydrogen $6/kg

    Laser $50 B (written off in 5 years)

    $10 B/0.5 B kg is $20/kg

    $36/kg, well under the $100/kg numberProfit more than $50/kg

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    Getting started

    (Building a seed laser) small scale, 500 MW @ 10 kg/kW

    5000 tons, Falcon Heavy @ 20 t per flight

    250 flights at 0.1 B/flight, $25 B

    $5 B laser at $10/W

    500 days at a launch every other day

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    Completing 3.4 GW

    $ 34 B laser/power sat parts, 17,000 tons

    60 scale vehicles, 5 tons to GEO

    20 flights per day, 170 days, 2 years total

    Transport cost @ $100/kg $1.7 B

    Total cost $50-100 BIncome @ $100/kg * 500,000 t $50 B/yr

    Payback from profit 3-4 years.

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    Falcons can't build power sats but

    they can build a large and

    expensive laser

    3.4 GW electric power at 2 cent per kWh is

    worth $480 M/yr

    3.4 GW of laser propulsion is worth $50

    B/yr

    >100 times as much

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    Part 4

    This makes a business case It closes the business case for making 2 cent

    per kWh power and we know there is plenty

    of market at that price (TWs) It solves energy, energy security and carbon

    problems (carbon neutral synthetic fuel for a

    dollar a gallon) Even at two cents per kWh it makes huge

    profits to support growth.

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    Growth: 100GW/year, ten percent (10

    GW) used for more propulsion,triples the cargo capacity to 1.5 M t/y,

    300 GW/year. Triple that and the

    expansion rate is almost a TW/year.

    It's possible that humanity couldbe mostly off fossil fuels in a

    decade. (If anyone cares, that is.)

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    It costs perhaps 10% of what a

    war with Iran would cost

    SDI with the USSR or Russia was/is a

    losing business. It will be decades before Iran could

    overwhelm a multi GW propulsion laser and

    by that time the commercial demand for

    laser propulsion should be in the tens of

    GW

    Cheap power from space removes any

    le itimate reason to sort out uranium atoms

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    BUTIt is too big to do without

    major government backing

    And oil, coal and gas industries will lobby

    against a real solution. (Maybe not) So why should a government consider

    backing it?

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    Google henson oil drum for a

    slightly out of date white paperon this topic

    Part 1 months ago

    Part 2 and 3 a few weeks ago

    Part 4 last week This is unlikely to be the final evolution of

    the idea.

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    Why Airdrop at 10 km

    Large Landing gear reduction

    Max landing is 54 tons, 120 t less 76 tons of

    LH2 dumped in an abort.

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    OVERALL CONFIGURATION OF GEOSYNCHRONOUS

    SPS (FROM DOE STUDIES)

    SPACEBORNE

    ARRAY

    RECTENNA ON

    EARTH

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