X-39

Future Aircraft Technology Enhancements (FATE)
Lockheed-Martin Study
FATE I PHASE I
FINAL REPORT BRIEFING

24 September 1997


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    Table of Contents

  1. PPT Slide
  2. PPT Slide
  3. PPT Slide
  4. PPT Slide
  5. PPT Slide
  6. PPT Slide
  7. PPT Slide
  8. Multi-Discipline Team Made Qualitative Assessment of Technologies
  9. PPT Slide
  10. Technology Matrix Format
  11. Five Technologies Selected for Study
  12. PPT Slide
  13. PPT Slide
  14. Technology Readiness Date
  15. PPT Slide
  16. PPT Slide
  17. PPT Slide
  18. PPT Slide
  19. PPT Slide
  20. Conformal Fluidic Nozzle
  21. Conformal Fluidic Nozzle
  22. PPT Slide
  23. PPT Slide
  24. Tailless Technologies Benefit Compared to 1995 SOA
  25. Benefits of Tailless Configuration Technologies
  26. Drag Reduction Potential of Tailless Designs
  27. Innovative Controls Can Replace Vertical Tails & Rudders
  28. All-Moving Wing Tips and Spoiler-Slot-Deflectors Are Weight-Efficient Tailless Controls
  29. Tailless Aircraft Risks/Penalties Compared with Those of Tailled Aircraft
  30. Tailless Aircraft TechnologiesRisks and Fallback Positions
  31. Continuous Aerodynamic Control Surface - CACS
  32. Flexible Structure Technology (FST) Enables Continuous Aerodynamic Control Surfaces
  33. CACS - Risks and Fallback Positions
  34. PPT Slide
  35. Advanced Wing Planforms - Lambda Wing
  36. Advanced Planforms - Risks and Fallback Positions
  37. PPT Slide
  38. PPT Slide
  39. Uninhabited VehicleSOA 1995 Technologies
  40. Uninhabited Vehicle2001 Technologies
  41. FWV Goal Benchmarking
  42. Output From Parametric Analysis
  43. PPT Slide
  44. PPT Slide
  45. PPT Slide
  46. Advanced Compact Inlet
  47. PPT Slide
  48. PPT Slide
  49. PPT Slide
  50. Advanced Wing Planforms: Lambda Wing (vs. Trapezoidal)
  51. PPT Slide
  52. PPT Slide
  53. PPT Slide
  54. PPT Slide
  55. PPT Slide
  56. PPT Slide
  57. PPT Slide
  58. Conclusions and Recommendations