Question:medium

In multi-stage rockets, the stage mass fraction is defined as

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For a rocket stage, \[ \boxed{ \text{Mass Fraction} = \frac{m_p}{m_{\text{stage}}}, } \] where \[ m_{\text{stage}} = m_p+m_s, \] \(m_p\) is propellant mass and \(m_s\) is structural mass.
Updated On: Jul 14, 2026
  • Ratio of payload mass to total rocket mass
  • Ratio of propellant mass to total stage mass
  • Ratio of total rocket mass to payload mass
  • Ratio of dry mass to payload mass
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The Correct Option is B

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