Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method and a system for launching satellites simultaneously on non-coplanar orbits by using highly eccentric orbits and atmospheric braking

Method and a system for launching satellites simultaneously on non-coplanar orbits by using highly eccentric orbits and atmospheric braking

US Patent 5961077 · Granted Oct 5, 1999

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Cryogenic liquid storage system for a spacecraft2014
Electrolytic igniter for rocket engines using monopropellants2013
Electrolytic igniter for rocket engines using liquid propellants2013
Emitter for ionic thruster2013
Closed electron drift thruster2012
Compression-evaporation system for liquefied gas2008
Cryogenic rotary coupling, and use thereof in particular in articulated fluid fe2005
Low-thrust cryogenic propulsion module2003
Closed electron drift plasma thruster with a steerable thrust vector2001
Closed electron drift plasma thruster adapted to high thermal loads2001
Method and a system for putting a space vehicle into orbit, using thrusters of h2001
Device for concentrating ion beams for hydromagnetic propulsion means and hydrom2000