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structural coefficient造句

"structural coefficient"是什么意思   

例句與造句

  1. Structural efficiency of a vehicle is maximized as the structural coefficient approaches zero.
  2. The structural coefficient ( \ lambda ) is a critical parameter in SSTO vehicle design.
  3. The structural coefficient is defined as:
  4. The curves vertically asymptote at the maximum structural coefficient limit where mission criteria can no longer be met:
  5. In some cases, we may label the arrow with its corresponding structural coefficient as in Figure 1.
  6. It's difficult to find structural coefficient in a sentence. 用structural coefficient造句挺難的
  7. This can be verified using the " single-door criterion ", a necessary and sufficient graphical condition for the identification of a structural coefficients, like \ beta, using regression.
  8. Given a mission profile \ left ( \ Delta v, m _ \ text { pl } \ right ) and propellant type \ left ( I _ \ text { sp } \ right ), the size of a vehicle increases with an increasing structural coefficient.
  9. If the reduced form model is estimated using empirical data, obtaining estimated values for the coefficients \ pi _ { ij }, some of the structural parameters can be recovered : By combining the two reduced form equations to eliminate " Z ", the structural coefficients of the supply side model ( a _ S and b _ S ) can be derived:
  10. In comparison to a non-optimized TSTO vehicle using restricted staging, a SSTO rocket launching an identical payload mass and using the same propellants will always require a substantially smaller structural coefficient to achieve the same delta-v . Given that current materials technology places a lower limit of approximately 0.1 on the smallest structural coefficients attainable, reusable SSTO vehicles are typically an impractical choice even when using the highest performance propellants available.
  11. In comparison to a non-optimized TSTO vehicle using restricted staging, a SSTO rocket launching an identical payload mass and using the same propellants will always require a substantially smaller structural coefficient to achieve the same delta-v . Given that current materials technology places a lower limit of approximately 0.1 on the smallest structural coefficients attainable, reusable SSTO vehicles are typically an impractical choice even when using the highest performance propellants available.

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