Mobile power system
A mobile power system comprises a plurality of energy sources, wherein at least one energy source is a solar powered generating device and at least one energy source is a wind powered generating device; a plurality of electronic and telecommunications components configured to receive the power generated by the plurality of energy sources and/or convert the power generated to direct current power; a plurality of batteries configured to store the direct current power; and at least one transportable housing configured to hold the plurality of energy sources, the plurality of electronic and telecommunications, and the plurality of batteries during transport of the housing, and wherein the housing is configured to remotely operate the at least one solar powered energy device and the at least one wind powered generating device when the mobile power system is in operation.
1. A mobile power system, comprising:
a plurality of energy sources, wherein at least one energy source is a solar powered generating device;
a plurality of electronic and telecommunications components configured to receive the power generated by the plurality of energy sources and/or convert the power generated to direct current power;
a plurality of batteries configured to store the direct current power; and
two or more Internal Aircraft/Helicopter Slingable series containers, each configured to selectively hold the plurality of energy sources, the plurality of electronic and telecommunications, and the plurality of batteries during transport, and wherein the two or more Internal Aircraft/Helicopter Slingable series containers are configured to remotely operate the least one solar powered energy device and the at least one wind powered generating device when the mobile power system is in operation,
wherein the Internal Aircraft/Helicopter Slingable series containers comprises a first end, a second end opposite the first end, a top wall, a first side wall, a second side wall opposite the first side wall, a bottom wall, and at least one opening disposed in the first end, the second end, the first side wall, the second side wall, the top wall, or a combination comprising at least one of the foregoing, and
wherein the at least one of the two or more Internal Aircraft/Helicopter Slingable series containers comprises a control room disposed in a rearmost portion of the housing opposite the at least one opening, wherein the control room is configured to house at least one of the plurality of electronic and telecommunications components.
2. The mobile power system of claim 1 , wherein the control room further comprises a cooling unit disposed in an end or wall at the rearmost portion, wherein the cooling unit is configured to control a temperature and a humidity in the control room.
3. The mobile power system of claim 1 , wherein the Internal Aircraft/Helicopter Slingable series containers satisfies International Organization for Standardization standards, Container Safety Convention standards, Coast Guard Certification standards, Military Specification standards, Mine Resistant Ambush Protected standards, or a combination comprising at least one of the foregoing industrial or military standards.