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Examples

  • A little difference nonetheless a rather important one (i.e. lift-to-drag ratio).

    Ares I Parachutes Test Successful - NASA Watch 2009

  • If we were to do it with a 15-tonne rocketplane (its wings will make the plane heavier) with a supersonic glide lift-to-drag (L/D) ratio of four, the mass ratio would be about five, so again 60 tonnes of propellant would be needed.

    The Case for Mars Robert Zubrin 1996

  • If we were to do it with a 15-tonne rocketplane (its wings will make the plane heavier) with a supersonic glide lift-to-drag (L/D) ratio of four, the mass ratio would be about five, so again 60 tonnes of propellant would be needed.

    The Case for Mars Robert Zubrin 1996

  • The key technical challenges of the HTV-2 program are the design of an innovative high lift-to-drag aerodynamic shape, advanced lightweight but tough thermal protection structures, materials and fabrication technologies, autonomous hypersonic navigation guidance and control systems, and an autonomous flight safety system.

    Space Business and Industry News at SpaceMart.com 2010

  • Officials say the HTV demonstrations were supposed to test enabling technologies that could eventually be employed by an operational system capable of prompt DARPA says the HTV craft features a high lift-to-drag aerodynamic shape, lightweight thermal protection structures and autonomous guidance, control and flight safety systems.

    SPACE.com 2010

  • The key technical challenges of the HTV-2 program are the design of an innovative high lift-to-drag aerodynamic shape, advanced lightweight but tough thermal protection structures, materials and fabrication technologies, autonomous hypersonic navigation guidance and control systems, and an autonomous flight safety system.

    Space Business and Industry News at SpaceMart.com 2010

  • The key technical challenges of the HTV-2 program are the design of an innovative high lift-to-drag aerodynamic shape, advanced lightweight but tough thermal protection structures, materials and fabrication technologies, autonomous hypersonic navigation guidance and control systems, and an autonomous flight safety system.

    TradingMarkets 2010

  • These technologies include an integrated Fly-by-Wire system that allows the engine/rotor/propulsor system to operate efficiently, with full control of rotor rpm throughout the flight envelope, high lift-to-drag rigid blades, low drag hub fairings, and Active Vibration Control.

    WN.com - Business News 2010

  • The key technical challenges of the HTV-2 program are the design of an innovative high lift-to-drag aerodynamic shape, advanced lightweight but tough thermal protection structures, materials and fabrication technologies, autonomous hypersonic navigation guidance and control systems, and an autonomous flight safety system.

    TradingMarkets 2010

  • Officials say the HTV demonstrations were supposed to test enabling technologies that could eventually be employed by an operational system capable of prompt DARPA says the HTV craft features a high lift-to-drag aerodynamic shape, lightweight thermal protection structures and autonomous guidance, control and flight safety systems.

    SPACE.com 2010

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