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  • Space Propulsion,
  • General,
• 29/10/2021

2. Inclusion of the Nozzle Divergence Angle into the Exhaust Velocity for Inertial Confinement Fusion (ICF) Space Propulsion & Jet Efficiency

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4. Relationship of limits in 1/x functions useful for optimisation of parameters in spacecraft design

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5. Basic propulsion equations for reaction engine type systems and link to jet efficiency

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