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Class 244/158.5 - Orbit insertion


Subclass of Class 244 - Aeronautics and astronautics
Definition: Subject matter including a process or specific means for
No. of applications: 12
Last issue date: 02/02/2012


Application No.Application TitleIssue Date
20120024136METHOD FOR LAUNCHING A MISSILE
An air-based vertical launch system is described by means of which ballistic missile defense can be achieved effectively from a large aircraft. A method for ensuring safe missile egress is proposed. A method for ensuring that the missile strikes the ballistic missile pa...
02/02/2012
20110272528METHOD AND SYSTEM FOR DELIVERING CARGOES INTO SPACE
A method for delivering space cargo including inserting one or more container spacecrafts (CSCs) into orbit. A CSC comprises a hull, a device for receiving cargoes (an artificial medium), a braking medium container, an arrangement for separating the cargoes and the brak...
11/10/2011
20100326045MULTIPLE-USE ROCKET ENGINES AND ASSOCIATED SYSTEMS AND METHODS
Multiple-use rocket engines and associated systems and methods are disclosed. A method in accordance with a particular embodiment includes launching a two-stage vehicle have a first stage and a second stage carried by the first stage. The first stage can be powered with...
12/30/2010
20100289342Space-Based Power Systems And Methods
Power supply satellites may be launched to LEO and boosted to GEO using power generated on board from solar insolation. A cluster of power production satellites may be operated as a phased antenna array to deliver power to one or more ground-based facilities, which may ...
11/18/2010
20100163683Space Elevator
A freestanding space elevator tower for launching payloads, tourism, observation, scientific research and communications. The space elevator tower has a segmented elevator core structure, each segment being formed of at least one pneumatically pressurized cell. The pres...
07/01/2010
20100108819METHOD FOR DESIGNING AN ORBIT OF A SPACECRAFT
A method is disclosed for designing an orbit of a spacecraft which allows the spacecraft to take a small-radius halo orbit near a Lagrange point while avoiding the prohibited zone where the spacecraft may be shadowed or might be prevented from making communication. The ...
05/06/2010
20100051750System and method for space elevator deployment
A system and method for the initial deployment of a space elevator using a tether, doubly spooled from each end, an inertial mass, beacon satellite and positional thrusters, whereby tether is de-spooled from geosynchronous Earth orbit altitude, using gravity and centrip...
03/04/2010
20090321578Planetary impact defense system
A system for defending a planet having a satellite against impact from an incoming body includes an explosive system and a propulsion system. The explosive system is adapted for deployment on the satellite and detonation thereon with sufficient explosive force to produc...
12/31/2009
20090251773LOW ORBIT MISSILE-SHAPED SATELLITE FOR ELECTRO-OPTICAL EARTH SURVEILLANCE AND OTHER MISSIONS
A low orbit optical imaging satellite has a long thin satellite body housing an optical telescope arrangement. A major part of the telescope arrangement has its optical axis roughly parallel to the direction of elongation and includes a mirror arrangement deployed to di...
10/08/2009
20090230249Method of Launching into Operational Orbit an Artificial Satellite and Associated Propulsion Device
A method is disclosed for placing a satellite in an operational orbit The satellite is equipped with its own satellite propulsion system as well as a detachable separate propulsion device The satellite and separate propulsion device are launched into a transfer orbit by...
09/17/2009
20090206204SPIN-STABILIZED LANDER
The invention provides a novel, low-cost, spin-stabilized lander architecture capable (with appropriate system scaling tailored to the attributes of the target) of performing a soft-landing on a solar-system body such as Earth's Moon, Mars, Venus, the moons of Mars, Jup...
08/20/2009
20090152402Satellite, method and a fleet of satellites for observing a celestial body
The invention concerns an observation satellite (1) which is intended to be placed in orbit around a celestial body (2), and which comprises a reflecting device (5), a receiving device (6), a linking mechanical system (19), the whole f...
06/18/2009
 
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