Design Desk Inc.

Geoengineering - Climate Change Mitigation

Asteroid Miner

The Asteroid Miner is a multi path aerospace engine platform that does not require fuel to function. The design uses a laser to bore into asteroids to obtain the metals contained. The system pressurizes the dome cap above the molten pool and causes the molten rock and metal to travel to a vacuum chamber where the slag is cooled. The design may be useful in asteroid earth impact mitigation as a fuel less mechanism then providing enough force to vector correct large asteroids. The design used in multiple units can then trench and cause molten material to channel a stream to the load lift system to then continually fill and cool the metal rich material. Blow back then prevented by angle of bore using the surface of the asteroid to confine the flow when molten material then traveling to the lift miner.

Parts List

1.  solenoid actuated oil flow valve multi port discharge with manual sheathed cable operation capacity

2. hydraulic flow return coupling

3. hydraulic fluid drain

4. voltage regulator

5. pneumatic pressure coupling and pneumatically pressurized  "oil" (silicone oil) electric oil flow control valve - with manual sheathed

    cable operation capacity

6. hydraulic fluid coupling

7. hydraulic fluid compression fitting

8. electric hydraulic fluid oil pump and filter assembly and oil level send pumps oil from under vacuum with one way valve upon the flow pipe

    to number 20 via electric motor (oil level sensor maintains oil level via signal and logic mapping electronic circuits to then adjust the solenoid

    controlled valve number 1)

9. vacuum tank with vacuum level sensor and oil fill cap The "vacuum tank" also then containing oil ( silicone oil )

10.  generator system  "start cycle" oil flow valve ( positional indicator sensor and positioned by the logic electronic circuit processor)

11.  drive chain and sprocket lubrication oil filter and oil pump assembly

12.  hydraulic fluid ( silicone oil )  hydraulic impeller tandem with the large sprocket

13.  sprocket and drive chain lubrication encasement ( non flammable non electrically conductive lubrication oil )

14.  hydraulic draft impeller - drives the armatures of the magneto and high voltage generator

15. magneto Ac ( alternating current electricity generator )

16. main high voltage generator

17.  electric motor and high speed gear set ( 1:20 ratio)  to cause higher rotation tandem with the high speed hydraulic fluid oil pump, number 18,

       to then induce the hydraulic draft effect in assistance with the compound drive chain and sprocket system

18. high speed hydraulic fluid pump tandem rotates with the r.p.m. ( revolutions per minute ) sensor

19.  rpm sensor

20. oil and air pressure pressure tank

21.  plasma box static electricity dissipation system

22.  high voltage management and electronic logic system  "mapping" circuits system control electronics

23.  particle accelerator control electronics

24.  levitation core depicted at

25.  perpendicular piston assembly location parts alignment depicted at

26.  perpendicular piston assembly location parts alignment depicted at

27.  perpendicular piston assembly location parts alignment depicted at

28.  perpendicular piston assembly location parts alignment depicted at

29.  plasma drive noble gas  "ion electric" electron propulsion focus venturi

30.  electron absorption rails inducts the electric current and particle accelerator to cause high pressure intake before the

       compression venturi and low pressure in the aft of the propulsion system

31.  ionized plasma (excited) diffusion - causes the heated plasma to enter the low press producing chilled return manifold

32.  plasma drive exhaust redirection valve assist in manifold pressure control

33.  solenoid valve control

34.  levitation core depicted at

35.  super cooler condenser (refrigeration condenser)

36. super cooler refrigeration system  (used to chill the plasma)

37. compression manifold feeds chilled plasma to the particle accelerator "coil" to then cause high "pressure" effect in the system before the

      internal discharge venturi - particle accelerator discharges to the plasma drive high pressure to cause high pressure at high velocity "feed rate"

38.  insulated "super cooler" evaporator chills the exterior of the manifold and is insulated

39.  vacuum chamber / negative pressure

40.  levitation core depicted at

41. pneumatic impeller

42. small sprocket

43. electron emitter

44.  pneumatic pressure flow guide

45.  pneumatic impeller tandem internal wheel causing the transonic propeller system to rotate and produce electricity "brush-less"

46.  electric pneumatic flow control valve

47.  pneumatic manifold pipe

48.  electricity management electronics

49.  compression pipe fitting

50.  magneto transonic compressor Ac Generator of electricity

51.  high speed ratio gear set (1:50) out put (high) tandem with number 52 high speed electric motor compressor propeller ratio

       gear set input tandem rotation with number 50

52.  electric motor transonic compressor electric motor upon the circumference

53.  field coil (augmented wire wound)

54.  field coil (augmented wire wound)

55.  vacuum system low pressure chamber

56.  high pneumatic pressure chamber

57.  compression pipe fitting

58.  compression pipe fitting

59.  shutter valve electric and hydraulic actuation

60.  compression propeller

61.  high speed gear set output rotation tandem with number 60

62.  high speed electric motor (dual shaft)

63. impeller transonic tandem rotating with the armature of the dual shaft electric motor and is the input of the high speed ratio

      gear set

64. pneumatic compression venturi

65.  venturi pressure safety valve

66.  high pressure pneumatic flow pipe

67.  valve control solenoid

68.  multi wire bus wire clip

69.  throttle valve

70.  de-compression baffle

71.  flow pipe

72.  vacuum manifold

73.  vacuum valve (electric and manual actuation via cable / lever and automatic safety contains vacuum level sensor)

74.  valve solenoid

75.  through port (bore hole)

76.  engine electronics electricity management "bay"

77.  vacuum level sensor and one way inert gas ( argon ) gas pressure fill valve * air works too....

78.  system electrical ground connects to the static electricity system contained within the electricity management control bay

       number 76

79.  hover motor Tv type ( system hull / casing is de-energized in number 76 static electricity inductance control system) - hull contains shock

       casing of compression laminate

80.  thru bore slip ring and servo motors (positions the vector of the sealed thrust jet)

81.  speed sensor

82.  pressure sensor

83.  horizontal plane rotator armature

84.  horizontal plane rotator field coil

85.  temperature sensor

86.  noble gas storage pressure tank

87.  electrical ground point

88. multi function inert noble gas valve  "fills" the plasma drive electron propulsion engine

89. electronics  "bay" and cooling fins

90. horizontal plane guide wheel

91. hydraulic / electric servo hinge  support arms landing feet sum of four

92. hydraulic / electric servo hinge

93. landing gear structural support with lighting and cameras

94. hydraulic / electric servo hinge

95. hydraulic / electric servo hinge mounting for the landing feet

96. landing feet with metal detectors

97. rubber tread

98. power  "thumb" with electric auger anchor screw

99.  anchor auger

100.  grapple tool toe (may dock laser used for trenching the molten rock metal for continual melt harvest)

101.  hydraulic elevator system - lowers the laser and molten magma intake carriage

102.  hydraulic piston elevator platform lift system

103.  clean out entry egress

104.  molten slurry holding bay

105.  out gassing / pneumatic pressure cycle

106. outer drop compression ring ceramic circumference air tight ring drops into molten ring to gas seal

107.  pneumatic "under dome" pressure feed causes the molten magma to rise into the vacuum chamber through the ceramic

         molten magma pipes

108.  ceramic lined magma uptake pipes - contains clean out lasers to clear the pipes after use

109.  high energy laser bank and shielded camera system

110.  dome drop hydraulics

111.  gas cycle system / cooling system

112.  hinge tool electric servo also able to melt drop ring to seal for out gassing control

113. pneumatic system gas control storage tank cooling chamber vacuum pumping (low) negative pressure when molten

        magma transfer

114. molten magma fill level sensor

115. pneumatic hose reel

116. transmitter receiver antenna

117. electrical power umbilical

118.  plasma compressor propeller electric motor - brush less

119.  transonic impeller P.M. ( permanent magnet  "magneto) Ac alternating current generator

120.  super cooler evaporator control - chills the electron plasma flow and electron inductance "absorption" system to "re-inject" the electron

         via electron emitter also control system for particle accelerator ie... rate of flow "throttle" reports to craft main navigation

         electronics / engine control "helm"

121.  mating bolt plate

Letter "A" =  spherical positional lifter sealed force vectoring electric pneumatic propulsion engine ( may be mounted about the circumference

                    on the exterior of the vessel hull to then aid in control of the additional weight of loaded vehicle additional system mounting then

                    on a rotational theta shape motorized carriage that allows for vertical lift or force to move a large N.E.O. (near earth

                    object ) - ie... Asteroid mitigation. The number 79 then mounted to the center of the theta allowing circular rotation.

Letter "B" = spherical positional lifter sealed force vectoring electric pneumatic propulsion engine

Letter "C" = vacuum producing system

Letter "D" = high pressure pressure "bubble" maintains constant air pressure in the chamber

Letter "E" = electric compound hyper thrust jet system

Letter "F" = vacuum chamber piped to letter "C"

Letter "G" = main levitation system depicted at

Letter "H" = landing gear hydraulic pumping system "bay" and redundant electricity producing generator systems

                    located at

Letter "I" = ribbon wire multi wire sensor bus system function feed current to logic processor main wire bus

Letter "J" = electron emitter refrigeration evaporator also chills the pressure chamber prior to compression venturi

Letter "K" = electron emitter - ionizes the inert plasma gas

Letter "L" = inert gas multi directional switch box contains temperature sensor

Letter "M" toroid magnetic focus electromagnetic

Letter "N" = ionized electron plasma flow stream focus electromagnet toroid

Letter "O" = venturi maximum pressure safety valve ( vents over pressure via electric valve actuation by solenoid and control electronic

                    circuit) system contains pressure sensor

Letter "P"= primary particle accelerator high gain plasma velocity plasma "pump"

Letter "Q" = "run" mode particle accelerator plasma velocity plasma "pump"

Letter "R" = refrigeration system condenser cooling fan electric motor ( brush less electric motor)

Letter "S" = refrigeration system cooling fan

Letter "T" =  exhaust manifold toroid electromagnet ( flow focus system)

Letter "U" = high range ratio gear set to wick the system forward a "draft effect" compound transonic electric jet engine number 118 causing

                   the acceleration of number 119 number 119 is the input side of the ratio gear set , number 118 the is the output of the 1:50 ratio gear set

Letter "V" = linear particle accelerator "idle tube"

Letter "W" = flow balance flow pipe also called the "prime draft particle accelerator" over pressure bypass flow channel then

                    venting  / discharging to letter "Q"

Letter "X" = particle accelerator "u" shape flow pipe

Letter " Y" = union bolt plate

Letter "Z" = multi wire "ribbon wire multi wire "bus" clip

Letter "1A" = return flow pipe may be chilled insulated chamber around the return flow pipe - the flow pipe is also center end point polar

                     array placement of multiple flow pipe ( ie... 4, 6, 12, 24 etc...), between the electric hyper jet exhaust ports equally spaced about

                     the circumference of number 39

Below please find a mote detailed description of the craft's systems.

* Note - the aft chamber number 39 then with internal baffle with tuned multi port about the circumference to exhaust the pressure flow - also the compound hyper jet / generator system containing number 118 and 119 then can be polar array from end point center point to then evenly evacuate the aft vacuum chamber number 39. Multitude of aft electric compound hyper jet / generator's then can be placed in increasing number equally spaced about the circumference sum of 4, 6, 8, 12, 24 etc... This allows for a more controlled force vector displacement. The said additional electric hyper jet  "array" then joining the intake of letter "Q" via tuned pipe intake "header". The connecting intake pipe "header" is also a particle accelerator to then guide the ionized plasma flow.

* Note - post number 29's shutter exhaust valve the chamber is chilled via a refrigeration evaporator upon the exterior of the casing between

             the casing and the high gain particle accelerator

* Note - additional flow bypass flow pipe from number 39 to number 37 will allow the electric compound hyper jet to remain within the

             mechanical properties. If additional magnetic stabilization for centrifugal warpage is designed within the electric hyper jet to

             prevent warpage from centrifugal motion (ie tensile strength of selection material) additional casing thickness is required to

             prevent projectile hazard from component failure.

Generator Description

In the schematic directly above the design system is a differentiation generator system implementing the hydraulic draft effect while "retaining " work potential to cause perpetual fuel less production of high voltage electricity.

Start sequence;

The operator then positions the valve lever connected to number 5 and number 1 to the "run position" causing pneumatically pressurized hydraulic fluid from the air pressure hydraulic oil pressure tank, number 20 to discharge into the vacuum /oil retainer tank number 9 with the pressurized oil flow traversing across number 41 causing the drive chain and sprocket system to rotate producing electricity.

The initial electricity production then allows for the operation of valve number 1 to actuate initially positioned to direct oil discharge to number 2 then changing position to direct oil back to number 20 after the electrical "re-introduction circuit" has become electrified. The electrical "re-introduction circuit" directs a percentile of generated electricity from number 15 and number 16 to the logic electronic control circuits, referencing number 19, and directs the produced electrical current to number 17's electrical drive motor.

This maintains the speed of the generator system.  Within the electronic control circuits the potentiometer / variable resistor has multiple settings to allow for different levels of electricity produced as per required by the operator's intent. The result is a hydraulic draft effect then returning the oil to pressurized confinement faster than the oil is discharge due to the oil pump, hydraulic impeller and drive chain / sprocket gear system's alignment. This is possible due to the "phase" of mass... hydraulic fluid in confinement, when pumped, acts as a solid and pneumatic "pressure" then flexes allowing the system to self re-pressurize. The generator uses the "work" potential without dissipating the work potential stored in the pneumatic pressure (air pressure). Number 8 maintains vacuum in the oil / vacuum retainer tank, number 9 and also force pumps the oil to confinement also by a percentile of generated electrical current from number 15 and number 16.

When the system is adjusted to produce high gain high voltage the valve number 1 is able to change position directing the oil flow to the air pressure / oil pressure tank also refilling the oil faster then the oil is displaced from the tank.

The vacuum level sensor also aids in the control of number 1's position to maintain and control the oil level and vacuum level in the the vacuum / oil retainer tank via the electronic control circuits in the logic processing electronic circuit board.

When the hydraulic pump number 18 is pulling oil from under high vacuum the vacuum level is increased and the system speed is increased. The vacuum tank "oil feed rate" is controlled by the valve number 5 also referencing the oil level float send in the vacuum / oil retainer tank number 9.

The excess produced electricity is then available, "baug" resistant and load reactive, to be applied to the design other functions.

* Note -  in the sealed electric propulsion system, number 79, the perpendicular re-introduction of pressure nullifies the resultant
              counter force in the thrust / force equation. This produces directional force vectoring for vessel hull  movement.

* Note - electric motors and generators are sealed gas type and explosion proof

* Note - the cycling pressurized inert Noble gas flow from number 88 to number 43 then chills the electron injection system and discharges post

             one way valve into the  "head chamber" of the plasma engine.  This aids in the temperature control the system with the temperature

             reading then attained in the mix head unit number Letter "N" containing the injector flow toroid focus magnet.