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 heat incurred when re-entry is incurred.
All magnetic fielding then dipole electromagnets with one pole sealed / insulated to cause correct shielding shape enveloping the vehicle
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 random resonance disruption for intake
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 resonance emitter. Upon the outer edge on both sides of the vehicle a vertical transmitter 1/2 circle emitter that may curl the
emission using different frequency to loop the emission in attempt to buffer the time dilation of the relativistic shear of the forward motion.
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 ) engine tool bay and air lock system (each side) for numbers 74,75, and 76.
( pitch and roll ) electromagnetic control surfaces magnetic propulsion system listed at https://www.designdeskinc.com/tilt-drive.html
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 electromagnet and transmitter shield emitter "shapes the plume" 360 degree emission dipole magnet "one" pole insulated
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. lock mounting up or down vector sealed pneumatic (argon) lift system engine listed
at https://www.designdeskinc.com/acorn-engine-system.html
75. lock mounting lock mounting up or down vector sealed pneumatic (argon) lift system
engine https://www.designdeskinc.com/acorn-engine-system.html
76. lock mounting 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 wave resonance emitter to vibrate apex focus - controlled electrical dissipation electrically insulated from the main hull
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 heat incurred when re-entry is incurred.
All magnetic fielding then dipole electromagnets with one pole sealed / insulated to cause correct shielding shape enveloping the vehicle
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 random resonance disruption for intake
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 resonance emitter. Upon the outer edge on both sides of the vehicle a vertical transmitter 1/2 circle emitter that may curl the
emission using different frequency to loop the emission in attempt to buffer the time dilation of the relativistic shear of the forward motion.
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 ) engine tool bay and air lock system (each side) for numbers 74,75, and 76.
( pitch and roll ) electromagnetic control surfaces magnetic propulsion system listed at https://www.designdeskinc.com/tilt-drive.html
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 electromagnet and transmitter shield emitter "shapes the plume" 360 degree emission dipole magnet "one" pole insulated
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. lock mounting up or down vector sealed pneumatic (argon) lift system engine listed
at https://www.designdeskinc.com/acorn-engine-system.html
75. lock mounting lock mounting up or down vector sealed pneumatic (argon) lift system
engine https://www.designdeskinc.com/acorn-engine-system.html
76. lock mounting 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 wave resonance emitter to vibrate apex focus - controlled electrical dissipation electrically insulated from the main hull
