Design Desk Inc.
Geoengineering - Climate Change Mitigation
Venus Atmospheric Repair Satellite
The following satellite design system will transmit a resonance signal into the atmosphere of the planet Venus to cause vibratory separation of Carbon Dioxide while also dimming solar gain by transmitted electron upon a carrier wave to reduce in coming solar gain. The system will ionize the random carbon causing the formed magnetically tilted molecules "heavy" to then ash out to the ground. Increased high altitude sulfur dioxide will form reducing the total solar gain in the process. The system then used also to
control re-enter de-funct satellites or clean space debris autonomously.
The remaining free radical Oxygen molecule will naturally then form ozone via intersection with ultraviolet light. The ionization transmitter then with 90 degree fold out (upon all 10 hexagonal hull), to cause electron upon diffused carrier wave to yield the atmospheric Sulfur dioxide and random loose carbon atom to "heavy re-combinate" compound with magnetic tilt into greater temperature and pressure by the resonance transmitter that emits loose electron, then causing the compound to ash out at higher temperature at lower altitude. The atmosphere on Venus is effectively a scrambled ocean chemically speaking. Using resonance to wiggle apart Sulfur Dioxide and Carbon Dioxide can yield loose Oxygen and loose Hydrogen to form water... and yes heavy in ph as the rain then acidic.... yet with dropping temperature organisms micro organisms (bacteria), can increase the ph.
The design day side orbital distance then able to effect total planetary hemisphere while in operation. The process will increase atmospheric lightning yielding "plasma destruction" and slight vitrification of the sulfur compounds while "ashing" out the carbon also sequestered within the vitrification composite. The vitrification composite then a "heavy" molecule / compound that falls to the surface of the planet effectively "cleaning" the atmosphere.
The particle accelerator then super cooled and with external magnetic permeable electromagnetic wrapping upon the toroid "ring" to cause magnetic field shielding for the internal electronics from high level radiation while obtaining safe magnetic level exposure for the internal of the craft. The magnetic poles upon the mirror line produced / adjacent particle accelerator "ring" electromagnet then magnetically aligned with opposite poles to cause dual magnetic field shield. (ie. controlled inductance with capacitance discharge static electricity low level electrical current dissipation system). Internal electrical system will use an artificial electrical ground (controlled electrical dissipation) to safety all electrical systems! Electrical systems will also use electricity surge suppression to safety the electrical components.
This effort then requiring ultra high levels of electrical production. To obtain this to function, the Inert Noble gas drive is then positioned so that a force static is obtained ie... "placed" so that the displacement vector then counter acts upon the displacement of the electric sealed force vectoring "lift jets" (letter "B"), to then compound the current in Letter "B" to maintain altitude / gimbal while being assisted to maintain positional "static" by the mobile sealed oil jets, number 18". The electricity production level that is then harvested from both the "lift jets" and the spherical position center "gas drive", letter "F", then feeding regulated current, at levels as per required for the system to operate as intended for the respective functions ie... systems transmitters, systems emitters, avionics (including engine speed / throttle control), and communications. The design "re-introduces" produced electrical current to increase total electrical output applied to work potential (thrust) and or governance "control electronics".
Parts List.
1. electric servo, "positional servo" with dual electricity transfer thru bore current transfer slip ring with positional sensor
2. oil jet sealed force vectoring navigation system
3. mounting system
4. oil jet flow system listed at https://www.designdeskinc.com/moon-scooter.html
5. high pressure pressure tank gravity spin dual component via electric motor contains fluid transfer slip ring used for zero gravity start function connects to number 4 via
flow pipe valve system for high pressure fluid pressure number 4
6. high pressure pressure tank high pneumatic pressure used for number 4, connects via pressure rated pipe with control valve system
7. Sulfur Dioxide resonance decomposition transmitter - transmits a pulsing vibration to wiggle apart the bond between Sulfur and the Oxygen molecule to cause thru the
ionization process a "recombined compound" then correcting the "thermal retention" and Ph (acidic), properties of the Sulfur Dioxide.
8. "Carbon Dioxide" resonance decomposition transmitter hinged lid.
9. hydraulic piston assembly "opens / closes" the shutter protecting the "Carbon Dioxide" resonance decomposition transmitter.
10. Carbon Dioxide resonance decomposition transmitter sum of six in 360 degrees left endpoint polar array
11. Sulfur Dioxide resonance transmitter sum of six in 360 degrees left endpoint polar array
12. combine particle accelerator and electromagnetic toroid electromagnet vessel shielding system
13. union mounting bolt plate assembly for both letter "A" and letter "C"
14. inert Nobel gas (Argon), filled ring pressure tanks used to fill or de-pressurize the "lift jets" letter "B" used for both letter "A" and letter "C". Component hard bolts
to the hull of the vessel
15. electron emitter - sum of 6 about 360 degrees, used to induce lightning within the atmosphere of Venus to cause lightning induce "plasma destruction" to increase
the sequestration of Sulfur by means of vitrification also then forming high level Ozone (O3) via the Ultraviolet light produced by the lightning itself.
16. electric motorized angular positional system for the electron emitter contains positional sensor and connection linkage.
17. internal induction protection (protects from induced current or radiation) for the system electronic control circuits temperature maintained includes chilling system contains
circuit controlled avionics / helm control - flight controls servo robot accessible, electrical relay system, circuit breaker system for vessel systems
18. oil jet mobile avionics trajectory vector unit also used to maintain orbital "static" while the vessel is in operation. Sum of four total units
19. oil jet and mounting system
20. frequency focus reflector bounces the transmitters signal
21. landing gear hydraulic piston system
22. landing gear leg beam
23. landing gear foot positional hydraulic piston stabilizer
24. landing gear foot positional hydraulic piston stabilizer
25. landing gear pivot
26. rubber landing gear foot tread - and electromagnet that hull contact's to a permanent magnet upon the hull's outer surface or used to stabilize and or the "grab" objects
intended to re-enter
27. particle accelerator electron emitter unit contains 12 electron injectors that feed velocity to the electron emitters, number 15, to "sink" to low altitude to cause
cloud based lightning to arc to the surface of the ground of Venus. This is required to cause the ground to act as an electrical ground.
28. internal servo robot arm maintenance services system - The unit can replace components do minor system functions adjustments uses an inter change grip (multi tool), to
then use multiple tool that are stowed number 29.
29. multi tool stow
30. servo robot accessible electronics bay redundancy avionics secondary
31. vessel hydraulic fluid pumping system, servo robot accessible
32. Carbon Dioxide resonance focus diffuser to "spread" the diffused transmission wave to cover wide swaths of the the atmosphere (total day side hemisphere)
33. "lift jet" injection manifold - unit contains 8 main pressure rated channel
34. high speed travel electromagnetic locking electromagnet - when in high speed transit the Ionization transmitter power hinge tilts the transmitter to lock the
transmitter and sensor bank to monitor active function / infrared / optical camera / spectrometer - sum of ten ( each surface), about 360 degrees so that the landing gear
is able to operate.
35. brushless generator transonic impeller (mid speed of the vacuum system that causes negative "pressure" in the lower half of the "lift jet" engine system).
36. brushless electric motor "compressor" transonic jet fan
37. high speed brushless electric motor "compressor" transonic jet fan
38. brushless generator transonic impeller causes increased mechanical speed in the compressor jet assembly, number 37
39. ratio gear system sealed chilled lubricant (silicone oil) cause alignment to increase speed of the rotating compressor number 35 (gear system at 1:4)
40. ratio gear system sealed chilled lubricant (silicone oil) cause alignment to increase speed of the rotating compressor number 35 (gear system at 1:4)
41. electric and hydraulic fluid actuated "lift jet" throttle valve unit controls the Argon flow speed exiting the system compression venturi
42. coil return tube - vacuum system causes low / negative pressure post "after" the venturi returning the gas at lower pressure to the thrust chamber providing constant
discharge pressure into vacuum causing vessel lift via sealed flow system. A mechanical balloon.... of sorts
43. vacuum flow manifold
44. electric drive motor for the base vacuum transonic electric compound hyper jet contains mechanical drive pneumatic impeller for mechanical running with 1:50 ratio gear
system to advance the compression vacuum jet fan system in addition to the electric motor drive system. Air pressure (Nobel gas pressure) obtained from the safety
regulator valve upon the "lift jet" venturi over pressure safety valve. The "50" of the ratio gear set then tandem to the input rotation of the "impeller" jet fan. The discharge
pneumatic pressure from the unit then enters the coil return flow pipe. Additional flow pipe (air pressure) 49 to 44. the impeller a dual inlet gate valve to pull air from vacuum
jet as well as the "re-directed" pressure flow from number 49. A dual stage impeller primary intake from vacuum jet flow second stage only when venturi pressure is at
specified pressure range. The second stage acting as a flow cycle mechanical engine speed "regulator".
45. revolutions per minute sensor (R.P.M. sensor) - used to "regulate" the electric motors speed and input electricity level
46. high speed compressor temperature sensor
47. high speed compressor
48. vacuum jet impeller drives the compressor fasted by argon velocity flow speed
49. "lift jet" overpressure safety vent valve electric actuation sensor information/ signal will auto adjust to slow system "lift jets" speed settings for safety
50. small receiving sprocket (2.5" dia.), drive air / vacuum producing pump
51. electric clutch references pressure and or vacuum pressure tanks levels for the zero gravity generator to operate correctly
52. air / vacuum producing pump
53. dual shaft electric motor drive shaft connects to mid size receiving sprocket (4" dia.)
54. 1:10 ratio gear set driven by the electric motor and receiving sprocket to produce 10 times the rotation speed to the hydraulic fluid pump number 55
55. high volume hydraulic fluid pump -induces system speed advancement via the "hydraulic draft effect" of a pressurized fluid pressurizing a tilt to then harvest angular
momentum as electricity while retaining the cyclical work potential as air pressure. Yielding sustained high voltage electricity production.
56. hydraulic impeller - the impeller is caused to produce rotation connected to the Magneto (electricity generator voltage regulated) and main high voltage
generator system internal speed limiter oil flow by-pass valve for the structural integrity of the connecting flow pipes to remain within their operating parameters
57. high voltage generator
58. permanent magnet magneto
59. large encased sprocket (12" dia.), drive sprocket via the retained work potential pneumatic pressure within the fluid (hydraulic fluid oil oil tumbler number 65).
60. generator system r.p.m. revolutions per minute sensor - information / signal used to adjust the generator stable speed
61. hydraulic fluid control valve - electric actuation valve contains system safety all stop function will prevent fluid lock
62. generator system vacuum tank
63. vacuum regulator valve with electric sensor to report actuation requirement / level / and temperature
64. dual component oil and air pressure "oil tumbler" electric "spin up" electric motor
65. dual component oil and air pressure "oil tumbler" pressure retaining pressure tank
66. pneumatic pressure pressure tank
67. pneumatic control valve electric "start system" valve - vents air pressure into the vacuum tank to cause the dual component oil tumbler
to rotate - required for zero gravity conditions
68. pneumatic impeller causes the oil tumbler to rotate via connecting hard bolt connection system (all generator components are "end drive shaft bearing
supported -sealed lubrication bearings with mounting housing for component stable placement)
69. radiation resistant hull - may use exterior "insulated balloons" with electric heat resistors filled with carbon graphite granule causing a water ice slurry for impact
resistance. Interior in hull water storage and pump system
70. Hinged impact safety shield Pv (photovoltaic), "solar panel" (inner surface), connects to systems electrical storage battery assist in system, "re-boot" tertiary "re-boot"
system functions sum of six panels upon the exterior surfaces upon the vessel end. Pv panels produce electrical current when the vessel is aligned toward the Sun when
impact shutters are positioned in the open position by electric hinge servo electric motors the electrical charging system for the battery bank fed electricity from the solar
panel also implements a piezoelectric solid state unit with battery charging capacity and an additional back up piezoelectric unit for systems clocks / inductance cage shielded.
71. one way valve
72. "gas jet" particle accelerator causes "return" inert noble gas to also cool as the speed is increased by "fluid stretching" the gas in increments similar to what an air
conditioner does in the evaporation cycle.
73. electrical and thermal insulation
74. venturi overpressure safety valves
75. gas jet venturi cause argon / refrigerant to increase in flow speed and discharge pressure
76. inert Nobel gas injector system sum of four in 360 degrees
77. throttle "head unit" a particle accelerator that will produce thrust from discharge injection unto linear flow of the flow cycle run speed of the inert Nobel gas
78. thermal cooling exchange system with electrical ground within letter "T" to "keep" the internal current "static electricity" within electrical load level for material selection
service parameter. Unit encasement of non-electrically conductive material electrically insulated from the structural mounting points.
79. control electronics "bay" servo robot service capacity
80. oil tumbler thru bore slip ring allows oil pressure discharge while maintaining pneumatic pressure
81. ionization transmitter hydraulic piston system position control mechanics
82. 1:50 ratio gear set input rotation via vacuum jet impeller (sealed lubrication)
83. landing foot hinge sum of four upon each quadrant
84. pressure rated vacuum hatch / entry hatch locking
85. refrigeration condenser
86. refrigeration evaporator
87. total hull embedded inductance "cage" prevents unwanted electric induction from disrupting sensitive electronics
88. circumference electric motor for the system draft compressor - a brushless electric motor to also be able to be used as a brushless electricity generator to feed current
to the internal coil particle accelerator
89. internal "throttle speed head" gas intake unit
90. six tube emitter "guide"
Label letter "A" = particle accelerator "ring" with wound electromagnet for magnetic shielding
Label letter "B" = lift jet - carbon graphite laminate composite with epoxy- high compression capacity for "pressurization" (perpendicular and circumference layering), as a
start pressure the pounds per square inch (p.s.i.) range the "lift jet" then pressurized to 1/2 the weight of the total vehicle with an inert non electrically
conductive Nobel gas such as Argon. Engine encased within a "shock casing" to protect from projectile and within an electrically grounded encasement.
One way gas (Argon), fill valve upon the pipe coupling.
Label letter "C" = particle accelerator for the solar diffuser system transmitters
Label letter "D" = Sulfur Dioxide resonance destruction emitter
Label letter "E" = electron emitter
Label letter "F" = spherical positional internal "gas jet system" . Total system electrical grounding / safe to the touch thermal and electrical. Interior electrically /
magnetically polarized surface repellant pole to prevent surface material etching by high speed gas flow within the engine system. The venturi exhaust gate
valves sum of two prevent "gas flow lock" whereas, the "shutter valve" / throttle" is then the main valve to accelerate the gas flow discharge. This feature
compensates for the compound vacuum electric jet suction preventing structural collapse of the main flow discharge chamber at velocity rate. A safety
feature for structural integrity.
Label letter "G" = solar gain diffusion transmitter system
Label letter "H" = sensor bank communications and avionics system, camera, proximity altimeter (landing system)
Label letter "I" = positional electric motor driven servo with thru bore current transfer slip ring and position sensor with avionics link via electric wire contains bearing
system (sealed lubrication)
Label letter "J" = gas jet bearing system
Label letter "K" = positional electric motor driven servo with thru bore current transfer slip ring and position sensor with avionics link via electric wire contains bearing
system (sealed lubrication)
Label letter "L" = left
Label letter "M" = core mounting system solid floor to roof pole
Label letter "N" = north polarity electromagnet "solar flare safety system" able to guide the flow and safely dissipate... to prevent damage from solar flare in sequence
shut off a magnetic pole to short the induction causes the flare to flip around
Label letter "O" = bearing system (sealed lubrication)
Label letter "P" = "gas jet" refrigeration system "refrigeration bay"
Label letter "Q" = electric magneto an Ac (alternating current), electricity generator also acting as a "drag break" to slow the compressor / impeller fans while producing
more electricity by the increased electricity level fed to the field coil of the unit causing rotational speed to slow "break baug". This keeps the centrifugal
elongation by rotation within the material selection service parameter.
Label letter "R" = right
Label letter "S" = south magnetic pole
Label letter "T" = "gas jet" gas / refrigerant injector electric discharges angular to cause step propulsion emitting 360 degree angular 30 degree toward center line flow
Label letter "U" = speed head particle accelerator able to within the unit can cause cyclical flow within itself to obtain extreme velocity causing high velocity
discharge unto center line flow yielding draft intake from return flow. The open center is a linear particle accelerator separate from the cyclical speed
head particle coil within the same unit. The cyclical speed head is pressure regulated with redundant valve (mechanical and electrical), with information
sensor reporting actuation level.
The "speed head" then discharges unto the center line gas flow using magnetic field dampener valve ie... "the internal
wound electromagnetic field changes strength to "guide" the gas flow speed either to the center line discharge or back into the coil that is then increasing
it's cyclical gas flow speed". High magnetic field = re-introduction / low magnetic field = discharge cycle to main line flow ie... "injects" high speed gas flow
to the center linear particle accelerator discharge plume.
Label letter "V" = venturi flow compressor
Label letter "W" = flare flow diffuser electromagnetic spread decompresses the gas flow by a spreading effect.
Label letter "X" = drive "input impeller" with thru center flow channel also a brushless electric motor. A brushless electric motor to also be able to be used as a brushless
electricity generator to feed current to the internal coil particle accelerator
Label letter "Y" = center input shaft gear system (automatic gear selection transmission) outer shaft then with greater rotational speed 1:150. The 150 of the
ratio then tandem with the transonic fan number 88. Center shaft tandem with the unit's dual shaft brushless electric motor who's opposite side output shaft
is then tandem rotating with letter "Q". The unit's electric motor then contains r.p.m. sensor (revolutions per minute sensor), and it's used to set the system
vacuum throttle.
Label letter "Z" = throttle system gate and shutter valve
* Note - The hydraulic draft generator system then twice within the vessel also using battery electricity to assist in start up via electrification of system drive electric
motor, number 53
* Note- The label letter "F" is then a depiction of the "gas drive" system. The component then requires an in depth description to assist in comprehension of it's function. Due
to the nature of the "gas drive" system... electricity produced from the flow cycle will need to be controlled as moving "fluid" / gas then produces static
electricity. The static electricity is harvested in letter "T" and directed to the electrical control unit number 79.
The electrical current level then conditioned (voltage regulated / and overload protected - waste current level dissipation injection speed discharge valve
position refrigerant flow speed / cold side refrigeration cycle speed) and directed to the master electronic / electricity management system within number 79, to "electrify"
the internal refrigeration system.
Letter "T" connecting coupling from the system thermal / cooling exchange system then is also an external port (one way valve with pressure level gauge), to "fill" the
"gas jet" with the required gas pressure / refrigerant level. Any excess electrical current that the design produces then is routed through the positional servo via thru
bore electricity transfer slip rings and directed to the vessel master power block number 30 where it (electricity) is directed to other vessel functions.
The "gas jet" speed head then a particle accelerator that can also use the static electricity harvest to cause cyclical (unto itself) internal speed advancement... producing
an increased speed of the inert Nobel gas within the unit. This allows for a "thrust" capacity to discharge as a "throttle" system increasing the speed of internal main
line center thrust flow until the venturi regulation over pressure sensors causes internal flow cycle speed limit, factoring venturi pressure level as a critical safety fault
within the system.
Letter "T's" system then contains a "run" speed flow cycle vent exhaust pressure dampener valve "set at discharge pressure level" while number 74 is feeding gas
pressure to the cooling exchangers. Number 74's "return" flow cycle then implements a pressure tank acting as a pressure "volume" sink (volume retainer), required for
the "speed pressure rate" to be maintained when accelerating the system with increase of the cold injectors, letter "T"
The discharge pressure valve of letter "T" will also be assisted by maximum pressure safety valve that vents a "run speed" level (base idle speed) ie... also
containing an information sensor to act as "level of actuation" of the valve to then communicate with avionics main logic "mapping electronics" to "govern" system
function. Vents unit "overpressure" into the venturi with the main valve open or closed. Collected information then reduces and extrapolates information via electronic
circuit to determine gas flow cycle speed producing a close estimate of velocity rate effect for the vessel's avionics information also displayed upon video screen placed
above servo robot base rotation servo with mechanical meter display (secondary avionics).
The electromagnets within the "return cycle" flow cycle use metal wire windings as the electrically conductive synthetic fiber has a thermal problem at required run rates...
*Note- The aft "decompression chamber in letter "F" then implements an over pressure safety valve that may be end point polar arrayed to then be in greater
number ie... the sum of 12 about 360 degrees to allow for greater chamber decompression. This becomes required to not encumber the flow speed within
the "gas jet" engine design. The aft transonic impeller compressor then has a speed limit factor (centrifugal elongation) and is regulated by the level magnetic
field coil strength in letter "Q" to act as a drag break yielding higher levels of output electricity production able to be directed to the internal particle accelerator in letter "F".
Material selection for letter "Q" is a critical factor ie... to be of ultra high tensile strength. The vacuum compound transonic draft electric jet within the aft of the
letter "F" is then able to induce greater magnetic levels within the circumference magnets (permanent magnets that are wound wire "pick ups), due to the static
electricity in the system internal gas flow. The electrical regulation system will be made to compensate for the effect. Produced electrical current then able to
be "re-introduced " to increase system gas flow speed in letter "F".
* Note - Between the landing gear mounted upon the hull resides the crafts main electrical generator system listed
at https://www.designdeskinc.com/utility-scale-fuel-less-power-plant.html then assisting in the power level for the particle accelerators / emitters / transmitters/ and
flight engines. The main generator scaled to mate to the hull also shielded in the same fashion that the hull is. This feature produces a "natural pendulum" by weight.
The design then able to meet the required load ( electrical ) requirement. The main generator then a "thin-line" version of the Magneto that is brushless for this
design. Motivated by the hydraulic draft effect of a pressurized fluid. The "hatch" number 84 is the service port for the generator as the hull is then bolt sealed
at it's mid- line. The voltage regulator can compound current or circuit switch voltage variable level to condition the electrical current for the components within the
vessel. Compounding current ie... to increase the field coils resistance by higher electrical current levels yielding increased total electrical output. Material selection
critical tensile strength a critical factor (elongation due to centrifugal motion). The main generator then implements a thru bore current transfer slip ring to direct
electrical current to the start / run electric motor also brushless. A dual generator system in one unit.
Description
The particle accelerator system will accelerate electron derived from free energy using the pneumatically pressurized draft of a rotating hydraulic fluid to then off set mechanical resistance while harvesting angular momentum converting it to electrical energy as electricity. The particle accelerator system will also feed electron at high velocity to the solar gain diffusion transmitter / watt per square meter reduction transmitter (also transmitting loose electron), and to the ionization transmitter system (also transmitting loose electron). Ground communications when in use uses a radio relay communications system due to the vessels placement ie... the day side of Venus.
The electron emission from both emitter systems then of "tight / narrow" diameter to induce electrical charge within the atmosphere causing lightning, while the "carrier wave" / ie... "the resonance decomposition "signal" a wider diameter. The ring particle accelerators are connected "so that", the bank of 12 electron injectors, number 27, feed electron to both particle accelerators letter "A" and letter "C". The particle accelerators may work linked or at differentiated speeds to increase total velocity of the emitted electron.
The inert Nobel gas (Argon), pressurized sealed electric pneumatic lift jet then similar to a mechanical balloon cycling high pressure to then discharge the force vectoring capacity into mechanically produce vacuum, causing sealed lift. The bank of two electric gas jet are mounted upon rotator carriage (spherical positional system), to then change the flight vector also assisted by multiple compound sealed fluid rhomboid fluid propulsion to assist in flight gimbal vector in a spherical fashion (mobile mounting spherical positional system). The gas jet system force vector displacement angle adjust by rotating in tandem or independently to cause vessel roll. Avionics fault safety to prevent overstress of the mechanical properties of the vessel ie... vessel speed dynamics limit trajectory correction (gas jet vector displacement), for systems safety. The oil jet system then used also to slowly slow high speed travel... as a retro trajectory function.
The solar gain reduction transmitter then not to in advertently affect (gauss) the asteroid belt or magnetize asteroids in the solar system disk plane.
The resonance transmitter to cause the bond between the carbon and oxygen molecules to vibrate apart yielding re-combinate sulfur compounds and atmospheric ozone. The ionized carbon will bond with the atmospheric sulfur compounds that are also present in the atmosphere. Carbon Monoxide will also form but can be cycled out after duration of system function. Atmospheric Nitrogen can be mechanically liberated from rock to increase the stability of the atmosphere over time or as an option the resonance system might be able to convert Carbon and Hydrogen to Nitrogen ion yielding Nitrogen.
Hull composite material selection then of metalized plastic whereas the dipped plastic is then coated with a metalized material that will allow for the thermal conductivity acting as an electric resistor to keep the plastic within service operating parameters. This reduces vehicle weight and embrittlement. The electromagnetics then are also of alternative material using an electrically conductive synthetic fiber to reduce weight. The scale of total system 20%-30% larger than a modern golf cart to allow for the power delivery vs. weight of mechanism to operate correctly. Metal is used in vehicle hull construction or only where required in components that service parameter demand it.
This is a cost effective method to, within a reasonable time frame, adjust the planetary atmosphere. If lift mechanism is used as a shuttle craft requiring an occupant the servo robot then also as a flight control yolk and safety locking upon the spherical positional "gas jet" system when in use. Internal atmospheric system within the electronics unit, number 17.
The vessel can be used as an asteroid capture vehicle then tethering a large net with multiple vehicle used. A cost effective "quick" response time method.
The Solar Gain Reduction system (solar gain diffuser) then may be good for re-directing an Earth bound solar flare and or to prevent a solar C.M.E. (Coronal Mass Ejection), Earth impalement advent. The vessel may also be used to compensate for the "Solar Dimming Effect" that will occur when switching off fossil fuels as the albedo effect feedback changes when atmospheric pollution particle falls out of Earth's atmosphere increasing the carbon dioxide's greenhouse effect intensity requiring a shorter response time frame.
* Note - the satellite has application for elemental conversion post resonance separation to cause water from the Hydrogen in the sulfur and the liberated Oxygen
if correct resonance sequence is applied. The Venusian atmosphere is an ocean if rearranged by resonance transmitter. Ph and particulate will stratify in deep pool
and can be force corrected to produce potable water using free energy with sufficient electrical power density applied using gravity as motive force. Motive
function via https://www.designdeskinc.com/gravity-desalination-plant.html
* Note - The design might have application regarding the Ozone hole above Antarctica "to resonate" CO2 causing free radical Oxygen to recombine into O3 (Ozone).
* Note - pilot entry egress (air lock) then a hatch mounted to the top center solar diffuser panel using a telescoping slide (diagonal travel motion), compartment large enough
to seat a person in a space suit.
* Note - The design will adjust final parameter once weights and measure is taken of system components ie... throttle valve gate orifice (wider diameter + dampener gate
valve for safety).
*
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Disclaimer - If attempting to produce these design yourself additional engineering may be required.. Design Desk Inc. will not be held liable. If you proceed with construction your self it's at your own risk... by use of "free to use systems" you acknowledge and accept the terms.. ( Please note not all systems contained here in have been released ).