Geoengineering - Climate Change Mitigation

Design Desk Inc.

 Interstellar Star Relativistic Shielding System

The inter stellar medium is a hazardous environment at high velocity. Transiting space at high velocity has many hazard including permeating radiation and micro object. The following design system is intended to cause the energy / material encountered to then be converted into shielding with minimal velocity disturbance.

By augmenting the collected micro particle and or radiation and redirecting it to then act as shielding for the same transitive or forward directional micro particle or cosmic ray radiation will cause "reactive" shielding then adjusting with assistance to the emission density. 

A feature of the shielding system is called the "Apex Lens" effect that polarizes and ashes the on coming random micro object while aligning the magnetic polarity of the medium being traversed. 

The hull design then incorporates a separator flight system listed at https://www.designdeskinc.com/sonic-automated-pollenator--mechanical-bee-.html and is able to re-enter atmosphere at slow velocity similar to helicopter descent speed. This reduces weight and is a safer method as the pilots then will not encounter excessive hear incurred when re-entry is incurred. 

Parts List

1. electromagnetic forward frame "cage induction dissipation" hard solid magnetic outer hull.

2. linear intake particle accelerator with magnetic induction inject intake velocity ash

3. linear particle accelerator

4. magnetic control surfaces causing lift or drop by pressurized hydraulics listed at https://www.designdeskinc.com/tilt-drive.html

5. impact shielded long range transmitter / receiver  direct high gain redundant video camera system / sensor bank "full spectrum"

6. recessed servo mounter long rang transmitter / receiver high gain

7. shield emitter tube insulated and encased for high speed impact "chilled" 

8. magnetic control surfaces causing lift or drop by pressurized hydraulics listed at https://www.designdeskinc.com/tilt-drive.html

9. forward hydraulic landing foot

10. exterior lamp system ( forward and perpendicular )

11. landing foot hydraulic pump system and safety locking break

12. high impact strength sliding canopy

13. canopy rail with electromagnetic and hard locking system / able to "retain atmosphere"

14. hoop ring to accommodate pilot's flight ball secondary helm

15. particle accelerator "swing arm" of air capable cold plasma drive listed

      at https://www.designdeskinc.com/cold-plasma-drive-toroid-static-compressor.html  contains louvered entry and can "run" on

      electrical compression only using electron repulsion

16. harvested atmospheric gases extracted from the shield system after gas spectroscopy and stratification for isolation allowing water

      or internal atmospheric storage , storage tanks

17. engine mount bracket system "heated to reduce thermal fatigue"

18. spherical positional mobile with https://www.designdeskinc.com/tilt-drive.html as the driver of magnetic propulsion

19. air capable cold plasma drive with seal able intake and exhaust shutter listed

      at https://www.designdeskinc.com/cold-plasma-drive-toroid-static-compressor.html 

20. intake shutter opened by electric servo and hydraulic fluid pressure operates in tandem with the aft exhaust shutter

21. aft shutter vent

22. open frame "air space"

23. aft landing foot hydraulic leveling system hydraulic cylinder fluid pumping system

24. hydraulic fluid pumping system

25.  sum of four trajectory lock magnetic spherical positional mobiles magnetic system listed

       at https://www.designdeskinc.com/tilt-drive.html 

26. shield harvest stratification and shield gas chilling system

27. high velocity particle accelerator allows for cyclical speed incline  allows for cyclical internal speed incline to emit at extreme velocity

28. linear particle accelerator ( final forward emission speed)

29. linear particle accelerator ( final forward apex lens emission speed)

30. aft intake electromagnet and injecting linear particle accelerator "collects and recycles" shield emission pressure

31. cross-over plumbing to allow for either or high velocity system to feed a balanced emission pressure

32. flow injection manifold

33. injection flow distributor

34. injection pump (linear particle accelerator)

35. stratified harvest injector system pulls from retained gas storage should the forward sensor detect a need for a denser

      emission to "thicken the shield when encountering a denser or more energetic radiation field

36. refrigeration evaporator (in tank) 

37. high speed gas pressure injection system

38. engine tool slide mounting bracket (used to bring an engine system into atmosphere for repair)

39. air lock system / slide tube

40. engine system port exterior electromagnetic and manual locking accepts the impact shield upon the separator flight vehicle listed

      at https://www.designdeskinc.com/sonic-automated-pollenator--mechanical-bee-.html  

41. aft open shield cycle open bore electromagnet / recycles aft shield pressure to force pump the collection back to the particle

      accelerator system

42. apex lens emitter to "cause" a cone focus at immense distance in front of the direction of travel to ash and magnetically align micro

      particle and feed the system so that the collection / harvest is then able to handle the flow correctly - polarization and ionization -thermal

43. engine servo grappling robot arm

44. tool servo robot (able to detach / unlock engine mounting systems)

45. powered swivel union

46. telescoping servo boom arm

47. powered servo swivel boom arm

48. under belly light and camera system ( sensor bank location )

49. engine boom ( also clamps the canopy when in high speed flight )

50.  boom locking recess

51. hydraulic drive system for the engine boom 

52. servo boom main drive motor and main pivot ( rotation by hydraulic fluid pressure and electric motor-sealed gas type)

53. exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure

54. exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure with camera and sensor bank

55. hydraulic pump system to motivate the canopy for the separator flight system listed

      at https://www.designdeskinc.com/sonic-automated-pollenator--mechanical-bee-.html

56. exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure

57. forward high gauss electromagnetic and transmitter shield emitter "shapes the plume" 360 degree emission

58. electrical generator system with cooler for the shield emitter hardware

59. vertical forward electromagnetic control surfaces (port and starboard) magnetic propulsion system listed

      at https://www.designdeskinc.com/tilt-drive.html 

60. perpendicular shield emitter 360 degrees

61. forward re-cycle emission to feed the envelope re-cycled density while to "funnel" the harvest 

62. atmospheric pressure storage tanks ( flow tubes to separator flight ball and air locked deck 67 main helm, Quarters, galley septic)

63. atmospheric pressure storage tanks ( flow tubes to separator flight ball and air locked deck 67 main helm, Quarters, galley septic)

64. chilled vessel shield pressure storage tanks

65. https://www.designdeskinc.com/cold-plasma-drive-toroid-static-compressor.html

66. plant bay horticulture

67. main helm air lock entry / contains atmospheric amine co2 ( Carbon Dioxide) scrubbing systems connects to H.V.A.C. systems

68. tool bay / electrical management hardware

69. air lock

70. atmospheric forward flight  "wing"

71. hull ground cycles induction

72.  flap flight control

73.  under deck electrical production compound wind generator system high voltage system ( under body contour vehicle exterior lifting surface)

74. up vector sealed pneumatic (argon) lift system engine listed at   https://www.designdeskinc.com/acorn-engine-system.html 

75. down vector sealed pneumatic (argon) lift system engine https://www.designdeskinc.com/acorn-engine-system.html

76. spherical positional mobile magnetic propulsion listed at https://www.designdeskinc.com/tilt-drive.html contains multi wire bus and

      positional system to force vector the vessel and maintain trajectory 

77. vessel elongation sensor limits craft speed for safety redundant 

78. exterior rear low profile air flight tail and rudder

79. spherical positional mobile magnetic propulsion listed at https://www.designdeskinc.com/tilt-drive.html contains multi wire bus and
      positional system to force vector the vessel and maintain trajectory / flight stabilizer - trajectory lock

80. rear hull air foil "wing" (above the aft deck) flap

81. rear hull air foil "wing" above the aft deck

82. internal ladder

83. Inducing hard forward - controlled electrical dissipation electrically insulated from the main hull

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