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METHOD FOR DELIVERING CARGOES INTO SPAСE AND A SYSTEM FOR IMPLEMENTATION OF SAME
Patent for invention RU2398717
(PCT/RU2010/000036 Pub. No.: WO/2010/08286)

The invention described below in several detalized variants makes space transportation more effective and inexpensive by using simple technics. Analogues of this invention are the container space craft of atmospheric air PROFAC of Sterge Dimitriadis and the container space craft of solid materials (CSC) of Edward Marwick.

Essence:

The subject of this invention is the system and the method for delivering raw materials and other simple substances to orbital stations and fuel depositories.

Unique advantages:

a) makes it possible -- using an orbital container device with thrusters - to increase cargo-capacity of modern space rockets up to 10-20 times;
b)makes it possible at substantially low cost (~$100/kg) to accumulate in space big stocks of raw materials to provide thermochemical rockets with fuel, space electrorocket engines (ERE) with working substance, orbital stations and space crafts with materials of anti-radiational and anti-meteoritic protection, landers with thermal protection materials, building of big space constructions out of elements created straight in the orbit, as well as for provision of orbital factories with silicon and other raw materials for production of solar batteries of space power stations of industrial scale.

The invention can be realized in different variants:

a)A CSC with elliptic trajectory and folding solar batteries.
b)A CSC with spiral trajectory and folding solar batteries with an engine arrangement (EA) on the basis of low-power EREs, or on the basis of an electrodynamic tether engine.
c)A CSC with cordless (fuel or accumulator) energy transmission to the EA from SB.
d)A CSC with a wired (cabled) energy transmission to the EA from SB.

The aforementioned variants are subdivided into the versions of the CSC to work with cargoes coming both from the Earth and from the Moon. At the same time lunar CSCs can be efficiently used to operate in circumterrestrial orbit in case of their usage in pair with suborbital rockets which accelerate cargoes for CSCs up to the speeds of 5500-6200 m/s.

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