Submission

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title
EMdriveCubeSats class 1M (10Ux10Ux10U=1m3) "mammy"
short description
EMdriveCubeSats class 1M (10Ux10Ux10U= 1m3) "mammy", is assigned to service CubeSats class 1U - 6U, and “clean space debris”.

Bio


Introduce yourself or your team
Denying all authority
Denying all gods and demons
I recognize only the laws of nature, which he himself has repeatedly verified ...
The singular truth that I accept without a doubt - "Before to deprive the life of God deprives the mind ... Before God deprives the mind of depriving the sense of humor ... If you have a problem with humor - think about the rest of your life"
What makes you an ideal candidate for this Challenge?
"The teacher of the theory and practical designing EM-drive"

Solution


Describe your solution.
EMdriveCubeSats class 1M (10Ux10Ux10U= 1m3) "mammy", is assigned to service CubeSats class 1U - 6U, and “clean space debris”. Has on board one or several EM-drive propulsion, which provide movement in any direction, several manipulators with video cameras for servicing 1U-6U, special connectors (slot) for reading and updating programs 1U - 6U. Equipped with high-power solar panels, battery compartment, control and communication unit, space monitoring unit.
What is the size of your proposed solution?
Based on the name "CubeSats class 1M (10Ux10Ux10U=1m3)" of the main body dimensions - = 1m3 but is equipped with 4 unfolding solar panels of high power - up to 10 kW, and with several manipulators that can go far beyond the dimensions. If it is necessary to obtain a large pulling force, several modules are docked. The total mass can be from 400 to 1200 kilograms.
Does your solution help Special Operations Forces missions? How?
Maintenance CubeSat - switching on / off the work, reading information, updating the program, replacing individual parts and batteries, additional power mode, additional information encoding or information transfer using a narrow beam antenna, transporting CubeSat from one orbit to another, removing CubeSat from Orbits, the removal of space debris and objects that interfere with the mission.
The most important advantage of this satellite is that it absolutely does not require a propellant and is capable of continuously moving in space at maximum power for 15 years.
Where known, identify platform accommodation requirements for power.
EMdrive propulsion is located on the sliding console, solar panels on 4 rotating swivel consoles for maximum power regardless of the position of the housing 1M. Communication, control and orientation blocks in the space, power management EMdrive, batteries are located inside the main body.
Where known, identify platform accommodation requirements for thermal control.
The main temperature control in the battery, the EM-drive control unit and the EM-drive main parts.
Where known, identify platform accommodation requirements for data transfer rate.
Since 1M has a large capacity and dimensions, it can be equipped with equipment much faster than CubeSat 1U
Where known, identify platform accommodation requirements for data transfer volume (per orbit).
Since 1M has a large capacity and dimensions, it can be equipped with equipment much faster than CubeSat 1U
Where known, identify platform accommodation requirements for bus stability and attitude control.
For orientation in space, a ready-made serial unit for satellites of the same weight and dimensions can be used.
Can you identify any additional platform accommodation requirements for your solution?
The presence of batteries capable of operating in a high-discharge / charge mode for at least 3 years, followed by their replacement in orbit.
Can your concept can be implemented with current state-of-the-art flight-qualified components, or will it require additional development? Please describe.
The main number of components are used ready, excluding only the EM-drive propulsion and its control unit. The existing theoretical calculation allows calculating and manufacturing an EM drive with a driving force from 0.01Newton to 10.000Newton with very high accuracy. Therefore, the calculation, manufacturing and testing of a specific EMdriveCubeSats class 1M should be performed relying on other parts of the satellite.
The theory, calculation, manufacturing and testing of the EM drive for EMdriveCubeSats class 1M are not included in the CubeSat Challenger and do not participate in the competition. These tasks are handled jointly with NASA in a separate project.
Intellectual Property: Do you acknowledge that this is only the Concept Phase of the competition, and all ideas are to remain the property and ownership of USSOCOM for future discretionary use, licensing, or inclusion in future challenges?
Yes

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