| 摘要 |
FIELD: lunar space power supply technology. SUBSTANCE: proposed method of lunar space power supply is realized with the aid of transmitting lunar energy antenna of type of multibeam active phased array emitting SHF energy generated by transformation of D.C. or A.C. energy from solar batteries in assembly of transmitters simultaneously in direction of receiving ground energy stations (rectennas) located on side of the Earth visible from the Moon and in direction of space near-earth ground orbital re-reflectors of SHF energy for its re- reflection to receiving ground energy stations (rectennas) located on surface of the Earth invisible from the Moon. It is proposed to divide transmitting lunar energy antenna (phased array) into two separate parts to ensure compatibility of characteristic dimensions of rectennas located on sides of the Earth visible and invisible from the Moon and decrease of characteristic dimensions of space near-earth orbital re-reflectors. One part is used to transmit SHF energy to receiving ground energy stations (rectennas) located on side of the Earth visible from the Moon, the other part is meant for transmission from them to receiving ground energy stations (rectennas) located on side of the Earth invisible from the Moon. Such division of common energy transmitting antenna provides for compatibility of characteristic dimensions of rectennas located on sides of the Earth visible and invisible from the Moon and for decrease of characteristic dimensions of space near-earth orbital re-reflectors to technically acceptable dimensions with preservation of high efficiency of transmission of SHF energy from the Moon to ground and near- earth space energy services, simplifies functioning and phasing of facilities of lunar space power supply, substantially reduces scanning angles of two separate parts of common transmitting lunar energy antenna (phased array). Apart from this there is ensured compatibility of characteristic dimensions of receiving ground energy stations (rectennas) with dimensions of space solar energy stations which are presumed to be placed into geostationary orbit and were developed before. EFFECT: improved functional reliability of method. |
