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 Sonic Automated Pollenator 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
- electromagnetic forward frame “cage induction dissipation” hard solid magnetic outer hull.
- linear intake particle accelerator with magnetic induction inject intake velocity ash random resonance disruption for intake
- linear particle accelerator
- magnetic control surfaces causing lift or drop by pressurized hydraulics listed at Tilt drive
- impact shielded long range transmitter / receiver direct high gain redundant video camera system / sensor bank “full spectrum”
- recessed servo mounter long rang transmitter / receiver high gain
- shield emitter tube insulated and encased for high speed impact “chilled”
- magnetic control surfaces causing lift or drop by pressurized hydraulics listed at Tilt drive
- forward hydraulic landing foot
- exterior lamp system ( forward and perpendicular )
- landing foot hydraulic pump system and safety locking break
- high impact strength sliding canopy
- canopy rail with electromagnetic and hard locking system / able to “retain atmosphere”
- hoop ring to accommodate pilot’s flight ball secondary helm
- particle accelerator “swing arm” of air capable cold plasma drive listed at Cold Plasma Drive “Toroid Static Compressor” contains louvered entry and can “run” on electrical compression only using electron repulsion
- harvested atmospheric gases extracted from the shield system after gas spectroscopy and stratification for isolation allowing water or internal atmospheric storage, storage tanks
- engine mount bracket system “heated to reduce thermal fatigue”
- spherical positional mobile with Tilt drive as the driver of magnetic propulsion
- air capable cold plasma drive with seal able intake and exhaust shutter listed at Cold Plasma Drive “Toroid Static Compressor”
- intake shutter opened by electric servo and hydraulic fluid pressure operates in tandem with the aft exhaust shutter
- aft shutter vent
- open frame “air space”
- aft landing foot hydraulic leveling system hydraulic cylinder fluid pumping system
- hydraulic fluid pumping system
- sum of four trajectory lock magnetic spherical positional mobiles magnetic system listed at Tilt drive
- shield harvest stratification and shield gas chilling system
- high velocity particle accelerator allows for cyclical speed incline allows for cyclical internal speed incline to emit at extreme velocity
- linear particle accelerator (final forward emission speed)
- linear particle accelerator (final forward apex lens emission speed)
- aft intake electromagnet and injecting linear particle accelerator “collects and recycles” shield emission pressure
- cross-over plumbing to allow for either or high velocity system to feed a balanced emission pressure
- flow injection manifold
- injection flow distributor
- injection pump (linear particle accelerator)
- 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
- refrigeration evaporator (in tank)
- high speed gas pressure injection system
- engine tool slide mounting bracket (used to bring an engine system into atmosphere for repair)
- air lock system / slide tube
- engine system port exterior electromagnetic and manual locking accepts the impact shield upon the separator flight vehicle listed Sonic Automated Pollenator “mechanical bee”
- aft open shield cycle open bore electromagnet / recycles aft shield pressure to force pump the collection back to the particle accelerator system
- 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.
- engine servo grappling robot arm
- tool servo robot (able to detach / unlock engine mounting systems)
- powered swivel union
- telescoping servo boom arm
- powered servo swivel boom arm
- 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 Tilt drive
- engine boom ( also clamps the canopy when in high speed flight )
- boom locking recess
- hydraulic drive system for the engine boom
- servo boom main drive motor and main pivot ( rotation by hydraulic fluid pressure and electric motor-sealed gas type )
- exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure
- exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure with camera and sensor bank
- hydraulic pump system to motivate the canopy for the separator flight system listed at Sonic Automated Pollenator “mechanical bee”
- exterior engine servo boom lock electromagnetic and manual hard lock by hydraulic fluid pressure
- forward high Gauss electromagnet and transmitter shield emitter “shapes the plume” 360 degree emission dipole magnet “one” pole insulated
- electrical generator system with cooler for the shield emitter hardware
- vertical forward electromagnetic control surfaces ( port and starboard ) magnetic propulsion system listed at Tilt drive
- perpendicular shield emitter 360 degrees
- forward re-cycle emission to feed the envelope re-cycled density while to “funnel” the harvest
- atmospheric pressure storage tanks ( flow tubes to separator flight ball and air locked deck 67 main helm, Quarters, galley septic)
- atmospheric pressure storage tanks ( flow tubes to separator flight ball and air locked deck 67 main helm, Quarters, galley septic)
- chilled vessel shield pressure storage tanks
- Cold Plasma Drive “Toroid Static Compressor”
- plant bay horticulture
- main helm air lock entry / contains atmospheric amine CO2 ( Carbon Dioxide) scrubbing systems connects to H.V.A.C. systems
- tool bay / electrical management hardware
- air lock
- atmospheric forward flight “wing”
- hull ground cycles induction
- flap flight control
- under deck electrical production compound wind generator system high voltage system ( under body contour vehicle exterior lifting surface)
- lock mounting up or down vector sealed pneumatic (argon) lift system engine listed at Acorn Engine System
- lock mounting lock mounting up or down vector sealed pneumatic (argon) lift system engine Acorn Engine System
- lock mounting spherical positional mobile magnetic propulsion listed at Tilt drive contains multi wire bus and positional system to force vector the vessel and maintain trajectory
- vessel elongation sensor limits craft speed for safety redundant
- exterior rear low profile air flight tail and rudder
- spherical positional mobile magnetic propulsion listed at Tilt drive contains multi wire bus and positional system to force vector the vessel and maintain trajectory / flight stabilizer – trajectory lock
- rear hull air foil “wing” (above the aft deck) flap
- rear hull air foil “wing” above the aft deck
- internal ladder
- Inducing hard forward wave resonance emitter to vibrate apex focus – controlled electrical dissipation electrically insulated from the main hull
