AIAA SPACE 2009 Conference &Amp; Exposition 2009
DOI: 10.2514/6.2009-6655
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Propellant Mass Fraction Calculation Methodology for Launch Vehicles and Application to Ares Vehicles

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“…Since typically more than 90% of the mass required for chemical rocket propulsion systems (such as hydrogenoxygen combustion engines) is propellant [5], the highest priority in space resource utilization is to make and use propellants in-situ. Large mission mass savings will result since the deep gravity well of the Earth, which accounts for 9.3 -10 km/s of delta-velocity to reach low Earth orbit from Kennedy Space Center at an orbital inclination of 28 degrees, can be avoided.…”
Section: Regolith Excavation Needsmentioning
confidence: 99%
“…Since typically more than 90% of the mass required for chemical rocket propulsion systems (such as hydrogenoxygen combustion engines) is propellant [5], the highest priority in space resource utilization is to make and use propellants in-situ. Large mission mass savings will result since the deep gravity well of the Earth, which accounts for 9.3 -10 km/s of delta-velocity to reach low Earth orbit from Kennedy Space Center at an orbital inclination of 28 degrees, can be avoided.…”
Section: Regolith Excavation Needsmentioning
confidence: 99%