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Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit [microform] / Joseph M. Roche and Daniel N. Kosareoval ([NASA technical memorandum] ; NASA/TM-2001-210667)

Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit [microform] / Joseph M. Roche and Daniel N. Kosareoval ([NASA technical memorandum] ; NASA/TM-2001-210667)
マイクロ図書
2001<YCA-NAS 1.15:210667>
国立国会図書館
  • 件名Air breathing boosters Reusable launch vehicles Prop...

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)
マイクロ図書
2001<YCA-NAS 1.15:210567>
国立国会図書館
  • 件名Air breathing boosters Hypersonic speed Computationa...

NASA Glenn Research Center's hypersonic propulsion program [microform] / Donald T. Palac (NASA/TM ; 1999-209185)

NASA Glenn Research Center's hypersonic propulsion program [microform] / Donald T. Palac (NASA/TM ; 1999-209185)
マイクロ図書
1999<YCA-NAS 1.15:209185>
国立国会図書館
  • 件名Air breathing boosters Air breathing engines Launch ...

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