Statite: spacecraft that utilizes sight pressure and method of use
US5183225A · kind A · utility
Inventor
Key dates
| Filing date | Jan 9, 1989 |
| Grant date | Feb 2, 1993 |
| Priority date | — |
| Expiry date | Jan 9, 2009 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64G1/407
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An artificial space object capable of operating usefully adjacent to, but not in orbit about, a celestial body such as the Earth, comprising: payload means for providing useful services from a position in space adjacent to the Earth, light pressure propulsion means for intercepting light pressure and directing the resulting force to oppose the gravitational force between the Earth and the space object; and attachment means for attaching the propulsion system to the payload, whereby the force generated by the propulsion system may be transmitted to payload. The invention is designated a "Statite", i.e. a useful space payload maintained by light pressure in a position adjacent to the surface of a celestial body, but not in orbit around it. The propulsion system may be a solar sail or it may be a solar photon thruster. The useful payload may be the space segment of a communications, broadcasting, remote sensing, or any other useful space system. The invention also teaches several methods of operating a Statite including polar and near polar positioning; solar orbital positioning; and halo orbit positioning.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.