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Central Intelligence Agency · 1990-01-01 · 53 pages · text by GLM-OCR

This Central Intelligence Agency file is a 1991 JPRS translation, report JPRS-USP-91-005. It carries the annotation and text of a Soviet brochure on the space program, written by one of the first cosmonauts. The brochure reviews what manned and unmanned spaceflight have achieved and calls the American lunar program a costly dead end pursued for prestige. It then proposes future tasks, including environmental monitoring satellites, orbiting factories, an international monitoring system, Mars sample return, radio telescopes and space robots.

  • p. 6 …fragments fall to Earth. If the altitude of the injection orbit is low (less than 200…
  • p. 12 …Such operations include studies performed with space telescopes placed in circumsolar and near-Earth orbits and…
  • p. 15 …Inexpensive reusable transport systems for transport operations between low orbit and geostationary orbit. 126. 18. Space…
  • p. 21 …Radio telescopes in near-Earth orbits or, what is more effective, in Sun-satellite orbits may…
  • p. 24 …glance, to offer important advantages over Earth-based and orbital telescopes. 169. The last task could…
  • p. 33 …acceleration from a low, near-Earth orbit to a high, injection orbit (beyond the Earth's…
  • p. 35 …injection of mission spacecraft into a low, near-Earth, assembly orbit, and use of transport craft…
  • p. 36 …communications with Earth, the mission module, and the Mars rover (via the orbiter). 247. Because of…
  • p. 37 …Based on a cost of $5,000/kg to put a payload into low orbit, using…
  • p. 39 …The booster-rocket stage must lift the spacecraft from a low, near-Earth orbit to an…
  • p. 40 …from Earth in a transport spacecraft that travels between Earth and the low-orbit servicing station…
  • p. 41 …travels between Earth and orbit and the costs of operating the low-orbit servicing station, which…
  • p. 42 …cost of putting the cargo into low, near-Earth orbit were assumed to be $5,000…
  • p. 52 …Low-orbit systems of standardized satellites for environmental monitoring, studies of natural resources, and weather observations…
  • p. 53 …low orbit and geostationary orbit. 353. 10. Space robots for operations in open space in Earth…

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Document 5 of 10

138. Orbiting Solar Electric Power Plants

139. One possible direction in the development of space-based operations to meet the basic needs of mankind involves the creation of orbiting solar electric power plants for supplying energy to ground-based consumers. Solar energy can be converted into electrical energy in various ways. But the simplest and most natural for our purposes is to use semiconductor converters that transform sunlight energy into an electrical current, i.e., solar panels. We have already accumulated experience in their long-term operation in space. Silicon cells are usually used as the converters-thin, small (several centimeters square) wafers in which a potential difference arises as a result the photoeffect that is produced when sunlight strikes them. Only a very small amount of power is derived from one such cell. The energy conversion efficiency in such a converter is on the order of 10-12 percent. To make a practical power-supply source out of those cells, they are linked in a series-parallel circuit. As a result, from one square meter of solar panel, one can obtain a quantity of power on the order of 140-170 W. Of course, such panels produce a current only under solar illumination, and such a level of power is produced only if the Sun's rays are perpendicular to the surface of the panels. That is why on many space vehicles, special systems orient the solar panels to increase the derived power. When the vehicle passes in the shadow of the Earth, the instruments and equipment get their electrical power supply from storage batteries that had been recharged by the solar panels when the vehicle was outside the shadow.

140. Orbiting solar electric power plants would be useful for supplying Earth with electrical energy. The electrical energy produced by the solar panels could be transformed into radio waves and transmitted in the form of a narrow beam to a receiving antenna on the Earth's surface by the pencilbeam antenna of the orbiting electric power plant. The waves received on Earth could then be reconverted into electrical energy and sent to consumers. In order for orbiting electric power plants to have continuous and immediate communications with ground receiving stations, the orbiting plants are best placed in geostationary orbit.

141. The most important thing in the creation of orbiting solar electric power plants is to master building in space gigantic structures that must be lightweight and steerable in orbit. We could begin, for example, with the assembly of an openwork panel unit that is, say, 100 x 100 x 100 m. And then, by gradually linking such units to one another, we could increase the area of the structure to dozens of square kilometers. A panel 100 sq m in area could derive as much as 10 million kilowatts of power. Transmitting the energy back to Earth from such an orbiting electric power plant would require an

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FOIA release, from the cia-readingroom collection. The PDF is mirrored here; the original link is above. The text was read from the page images by GLM-OCR; expect the odd misread word. 53 pages are in the text index: search them above, or from the library's search.