Propulsion to Moons of Jupiter Using Heat and Water Without Electrolysis Or Cryogenics

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Propulsion to Moons of Jupiter Using Heat and Water Without Electrolysis Or Cryogenics Anthony Zuppero NeoKismet L.L.C. Space Exploration 2005 The First International Conference and Exposition on Science, Engineering, and Habitation in Space, and the First Biennial Space Elevator Workshop April 3-6, 2005 Albuquerque, New Mexico, USA

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Propulsion to Moons of Jupiter Using Heat and Water Without Electrolysis Or Cryogenics. Anthony Zuppero NeoKismet L.L.C. - PowerPoint PPT Presentation

Transcript of Propulsion to Moons of Jupiter Using Heat and Water Without Electrolysis Or Cryogenics

Page 1: Propulsion to Moons of Jupiter  Using Heat and Water  Without Electrolysis Or Cryogenics

Propulsion to Moons of Jupiter Using Heat and Water

Without Electrolysis Or Cryogenics

Anthony ZupperoNeoKismet L.L.C.

Space Exploration 2005The First International Conference and Exposition onScience, Engineering, and Habitation in Space,and theFirst Biennial Space Elevator Workshop

April 3-6, 2005Albuquerque, New Mexico, USA

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Nuclear Thermal Rocket

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NERVA rocket

Thank youMell Merrit

for inspiring me.~ 1971

Jackass Flats,Nevada

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Callisto, Ice Moon of Jupiter

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H2O NTRdoable now

LH2 NTR doable

someday

LH2 NTR doable now

10,000 10,000 10,000 tons useful payload

1,090 1,675 28,072 tons non-payload

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Lunar South Pole, by D.O.D. Clementine

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Water Extractor

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Lunar Hydrogen at Forever Dark Poles

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Near Earth Asteroidsyou

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Toutatis, near Earth

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Pcomet Wilson Harrington

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Periodic Comets= "Jupiter Family Comets"

= Short Period Comets

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Halley’s Comet

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Ice Moon Orbital Velocities ~ like Earth's Moon

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Earth Jupiter

Callisto

moon

Orbital Maneuvers

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Electricity In Space, or NOT

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H2O NTRdoable now

LH2 NTR doable

someday LH2 NTR doable now

10,000 tons useful payload

[ 358,000 ] [ 139,000 ] [452,000 ] tons water needed from space resources

358,000 15,400 50,300 tons propellant used

312 154 503 tons armored tanks

656 472 1538 tons Nuclear Thermal Rocket engines

122 48 156 tons hardware to extract water

0 559 10,248 tons electric generator for electrolysis

0 70 5,027 tons for cryolizer

0 372 10,600 tons electric generator for cryolizer

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H2O NTRdoable now

LH2 NTR doable

someday

LH2 NTR doable now

10,000 10,000 10,000 tons useful payload

1,090 1,675 28,072 tons non-payload

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At Maximum Power, You Choose Propellant Mass

Specific Impulse

NET

Payl

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