ShwayComs Cg-s4 - Magnetic Space Crane SL-02 SV: Magnetiska Hiss Rymdskeppen 1100368-8

 

The Earth's magnetic field, also called the geomagnetic field, which effectively extends several tens of thousands of kilometers into space, forms the Earth's magnetosphere. § Source Wikipedia

Constant field thirty to sixty grams magnetic pressure at surface area; solar storms can present windows of manifold magnetic pressure increase often of two to eight hours duration.

The earth's magnetic field is a strong one and is created by lunar rotation against it's geo dynamo. We don't think of it being that strong and it goes largely unnoticed. The reason that this can go on is due to shape and size plus comparitive immersion in it's field extending some 35,000 miles§ (USGS Open-File Report 99-132) into space resulting in a low field divergence for objects at the surface of the earth.

While this illustration is for the same static field, to the left, field lines have a low divergence and produce not much noticable force on a paramagnetic, to the right with a higher divergence a stronger force is produced by the same field for a magnetic ordered paramagnetic immersed in this field. The earths field is compared to be 10% that of common household refrigerator magnets.

 
 

Reliable compression thrusters can be included for increased mobility and lunar near space trips for a vessel. Key to building this is power to weight ratio – there is very good light weight battery technology around however if this is not possible then as with FP-01 one could resort to using a microwave rectenna inducer skirt underside laminate powered from a base station for the vessel. Ionized gas solenoid core constructs along with rapid discharge Li-ion energy source which would be a lot more flexible and cost effective compared with high density field guided and dispersed designated microwave base station. Gas exchange coil and core cooling should be considered and light weight isolation. We choose ionized gas solenoid construct because of its property of being extremely light and electro magnetic suitable. A core magnet can exhibit tonnes of magnetic pressure per square centimeter and ionized gas solenoid is much lighter than a lithium core; also a vehicle can have a shallow shelf ring of 5 or 1000 cores. Core constructs can have different configurations for packing as spiral, round coil wiring or triangle coil wiring with ventilation gas cooling shafts through, vertical or adjacent to the coil and solenoid core construct.

Solenoid lift:

Standard solenoid lift potential estimate one meter core surface area  
Earths magnetic field Gauss 0,5
Earths magnetic field Tesla 0,00005
Teslas B field square cm 1,6
Gauss B field square cm 16000,00
Lift magnetic surface area 60cm radius 11309,00
Bold magnetic pressure exerted gauss 180944000
Elevator magnetic pressure attrition gauss 90472000
Magnetic potential for lift in newtons 18094,4
Magnetic potential for lift in kilograms 1809,44
Elevator lift potential attrition standard solenoid single core (estimate) kilograms§§ 904,72
   
Metric tonnes 0,905

Solenoid weight est:

Cylinder core belt width
20
Cylinder core inner width
100
Cylinder outer inner width
120
Lithium ion weight standard
0,534
Core cylinder weight
184780
Helium helicity mechanism
unknown
Aerogel insulator
unknown
Core wiring
256,0899
Core cylinder
18,478
 
Metric tonnes 0,275

 

Calculation of estimates based on Gausian formulation and principles.

Any variety of energy sources could be employed at last look a retro rocket could be fitted to turbine generator genset. Recommended for this spacecraft is carbon graphite shell construct retractable shock absorbing aluminum pylons for landing. Spacecraft body shell engineers should be aware of diamagnetism exhibited by some graphite and attenuator enhancers of ferrous materials.

 

With this attitude gyro the vessel takes off while it is fully spinning as this is when a flip over is critical to avoid. Turning this gyro along the X axis will produce no force on the vessel just to point out in the omni roll design. It is flown as with a helicopter stick to influence the vessel with drag stabilizing and controlling attitude- a release deceleration of the gyro will cause the vessel to surge upwards radically. Exhibiting a force on the Z axis of the gyro will cause a attitude correction acting on the center of the mass of the vessel as the gyro creates an artificial drag on the center of mass . In this way with attitude control and sling shot acceleration the vessel paradigm as a X/Z attitude acceleration into space giving greater control versus a magnetic vessel without this gyro. The gyro can also be use as a training wheel on a tricycle; a vastly more stable and safer to fly vessel. Friction free magnetic bearings can be used for the gyro with slip clutches and brakes in construction along with basic opposition gearing as employed plates spin at equal rate of rpm spin .

 

Ionosphere checker Rectenna RF microwave fueled solar panel laser fueled

Yang Juan's EmDrive microwave research

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This vessel is called the space crane because it not only elevates off magnetic bodies like the earth also exhibiting crane like thermal flight dynamic along with crane like latitudinal responses at a static with tides. It can do this horizontally like a compass or at 90 degrees theoretically.

Requirement: Other than rocket propulsion of various types and solar sails there is no other proven technology existing for spacefaring. This is a unique breakthrough of process and methodology in logistical spacefaring which cannot be dismissed. The technologies employed exist where the practice, usage and conception did not; I claim ownership as proponent and originator of this concept step towards spacefaring having researched solutions.
 
 
 

Practical proapplication :

Ionized gas electric solenoid spacecraft magnetosphere propulsion would be a practical approach in putting up infrastructure for regular load carrying shuttle service routing to and from Mars (a highway) and lunar domestic cargo load bearing bi-direction with lunar minerals return cargo. There is the need to eventually develop terra forming scale technologies at the municipal level in order to maintain our own environment when thinking of our well being in the long term scheme of things ( 100,000 years ) . Degradation of things like loss of ozone belt may take place over hundreds of years but these threats are there and have consequences; this cited probably requires some sort of reconstitution. We would accomplish a great deal in my opinion if we can learn to thrive in a place like Mars where we could build biosphere communities as well as engage in productive self sustaining activities like exploration and adding to the wealth of everybody (things we have yet to uncover).

Having been in dialogue with noteworthy physicists on internet network meeting point; thier interest in this logistics was to suggest to look to getting helium 3,4,5,6,7 isotopes from the moon which would greatly simplify fusion reactors today supplying a significant municipal input of the earths energy requirement and releasing alpha helium elements (atmospheric bind) as a positive compliment. Apparently 22.7 tonnes of refined meta helium isotopes is suggested to be the required estimate of total yearly minicipal raw material reportedly; what volume of heliosphere this would contribute has yet to be evaluated from known ores estimated to concentrate at 67ppm resulting in a measure of 15 tonnes of haulage per kilogram of this mineral at that site. The composition of Uranus at 20 AU is thought to be of 3% helium yielding 30 kilos of refined helium ores per processed tonne of material , it also has a magnetosphere but presents harsh working environmental realities . Logistics ( transportation ) understanding of this alpha helium expansion initiative is that climatologist physicists would like to increase the radiating sink properties of the heliosphere positively affecting exosphere exposure green housing. Ethically I can't reason that lunar has ever had what are the requisite tour dynamics to have been habitable to consider this enterprize marauding.
 
During 2012 the US congress passed a $35 bn administration waver for a moon base establishment is a good example of progress, ESA, visible at Esrange and Kiruna Space Port extended fully open to enterprize several new and attractive packages.

NB: I have some magnetic schematics from Open Aero SpaceX which I am continually working on; submissions by interested parties to cg-s4.com appreciated.

NB: Energy projections to exosphere space may create radical adverse weather react conditions in the ionosphere.