New Aluminum-Ice Rocket Propellant Tested
eldavojohn writes "With the problem of moving conventional rocket fuel to the Moon and Mars on their minds, researchers from Purdue and Penn State successfully tested and demonstrated the use of aluminum-ice (ALICE) as fuel. In a paper from last August they outlined how it would work (PDF), and now they know it does. Space.com also has more information on the paper and how nano-scale aluminum functions as a fuel."
MIT Technology Review is a little late here. This was covered by numerous sources back in October. Surprisingly, I can't find it in the /. archives; so, it may not be a dupe.
For a neat visual presentation of the physics they're relying on, Mythbusters did an experiment on the explosive power of thermite powder and water vapor http://www.youtube.com/watch?v=BnHR4cMXiyM.
You may be too young to remember, but it was acceptable and even funny to beat your wife in the '50's.
Get off my lawn or one of these days...POW! Right in the kisser!
that highlight the safety instructions I've had at Aluminium plants. You never, ever, ever drop anything like used aluminium cans into the feed that is headed for melt shop as any bit of liquid still in the can will cause a rather powerful explosion
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Really? Because hydrogen is the most common element in the universe, and oxygen is also pretty close to the top of the list (third most abundant element overall). Comets contain a lot of water ice. Aluminium is on of the three most common elements in the Earth's crust, but it's not nearly as common as hydrogen and oxygen in the universe at large.
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Assuming a 2 to 3 Al to H2O molar ratio, it looks like the exhaust velocity is about 900 m/s so the Isp is about 90s.
: 1.458 g/cm^3
: 3166.569 : -7944.256 : -8685.762 : -33443.801 : 8.053 : 35.507 : 3.30500 : 3.00720 : 1.09903 : 1.09264
If that's right, that sucks compared to normal mixtures.
Of course, if you're lifting off the moon or asteroids, it may be ok. Mars? Probably not.
Computing case 1
Fixed enthalpy-pressure equilibrium - adiabatic flame temperature
Propellant composition
Code Name mol Mass (g) Composition
34 ALUMINUM (PURE CRYSTALINE) 2.0000 53.9631 1AL
976 WATER 3.0000 54.0458 2H 1O
Density
3 different elements
AL H O
Total mass: 108.008918 g
Enthalpy : -7944.26 kJ/kg
24 possible gazeous species
8 possible condensed species
CHAMBER
Pressure (atm) : 340.230
Temperature (K)
H (kJ/kg)
U (kJ/kg)
G (kJ/kg)
S (kJ/(kg)(K)
M (g/mol)
(dLnV/dLnP)t : -1.00584
(dLnV/dLnT)p : 1.13099
Cp (kJ/(kg)(K))
Cv (kJ/(kg)(K))
Cp/Cv
Gamma
Vson (m/s) : 900.11114
Molar fractions
AL 6.0290e-004
ALH 9.2486e-004
ALH2 2.8353e-005
ALH3 2.1470e-005
ALO 2.4478e-005
ALOH 5.6133e-003
AL(OH)2 3.4527e-005
AL(OH)3 3.1024e-006
AL2 1.4157e-006
AL2O 1.3669e-003
AL2O2 1.1545e-005
H 1.0276e-002
HALO 2.7342e-006
HALO2 3.5370e-007
H2 7.2954e-001
H2O 7.8723e-003
O 3.5048e-007
OH 4.1466e-005
Condensed species
AL2O3(L) 2.4364e-001
Seastead this.