Abstract

A core element for use with an inflatable or expandable spacecraft is claimed. The core element has a plurality of panels connected by hinges so that the core element can be packed into a smaller volume for loading into a launch vehicle. Upon deployment in space, the core element can be unpacked and can enclose a larger volume than that in the packed state. Multiple core elements can be used to cover a spacecraft to a desired degree.

IPC Classes  ?

• B64G 1/56 - Protection against meteoroids or space debris
• B64G 1/58 - Thermal protection, e.g. heat shields
• B64G 1/10 - Artificial satellitesSystems of such satellitesInterplanetary vehicles
• B64G 1/22 - Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles

Abstract

A spacecraft capture tug is disclosed. The tug can capture objects in space, including spacecraft and satellites, using an engagement system and provide propulsion for the object to a point of servicing, repair, or other desired operations. Further, the tug may dock with other specialty tugs to form a custom transport system.

IPC Classes  ?

• B64G 1/64 - Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
• B64G 1/40 - Arrangements or adaptations of propulsion systems
• B64G 1/42 - Arrangements or adaptations of power supply systems
• B64G 1/44 - Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
• B64G 1/12 - Artificial satellitesSystems of such satellitesInterplanetary vehicles manned
• B64G 1/26 - Guiding or controlling apparatus, e.g. for attitude control using jets

Goods & Services

DESIGN OF COMMERCIAL SPACECRAFT AND COMPONENTS USED IN SATELLITES, SPACECRAFTS OR SPACE SHUTTLES AND ENGINEERING IN THE AEROSPACE INDUSTRY