Characterization of nanoscale aluminum and ice solid propellants
TR Sippel - 2009 - search.proquest.com
Solid rocket motors are favored for launch applications because of their simplicity and high
thrust to weight ratio. Longer space missions and manned missions will require new, higher …
thrust to weight ratio. Longer space missions and manned missions will require new, higher …
Characterization of nanoscale aluminum and ice solid propellants
TR Sippel - 2009 - docs.lib.purdue.edu
Solid rocket motors are favored for launch applications because of their simplicity and high
thrust to weight ratio. Longer space missions and manned missions will require new, higher …
thrust to weight ratio. Longer space missions and manned missions will require new, higher …