ROGER XAVIER LENARD
Pilots at Dunkin Rd, Edgewood, NM

2004003, Feb 19, 2004

Nov 15, 2002

10/298138

Robert D'Ausilio - Bountiful UT, US
Roger Lenard - Edgewood NM, US
Bari Southard - Bountiful UT, US

B64G001/62

244/172000

An In Orbit Transportation & Recovery System (IOSTAR™) () is disclosed. One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (). The IOSTAR™ includes a collapsible boom () connected at one end to a propellant tank () which stores fuel for an electric propulsion system (). This end of the boom () is equipped with docking hardware () that is able to grasp and hold a satellite () and as a means to refill the tank (). Radiator panels () mounted on the boom () dissipate heat from the reactor (). A radiation shield () is situated next to the reactor () to protect the satellite payload () at the far end of the boom (). The IOSTAR™ () will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.

7070151, Jul 4, 2006

Jan 9, 2004

10/755200

Robert F. D'Ausilio - Bountiful UT, US
Roger X. Lenard - Edgewood NM, US
Chauncey W. Uphoff - Longmont CO, US

IOSTAR Corporation - North Salt Lake City UT

B64G 1/10, B64G 1/40, B64G 1/64, B64G 1/54

2441711, 2441724, 2441717, 2441722

An In Orbit Transportation & Recovery System (IOSTAR™) () One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (). The IOSTAR™ includes a collapsible boom () connected at one end to a propellant tank () which stores fuel for an electric propulsion system (). This end of the boom () is equipped with docking hardware () that is able to grasp and hold a satellite () and as a means to refill the tank (). Radiator panels () mounted on the boom () dissipate heat from the reactor (). A radiation shield () is situated next to the reactor () to protect the satellite payload () at the far end of the boom (). The IOSTAR™ () will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.

7645437, Jan 12, 2010

Oct 17, 2007

11/873451

Robert Moore - Edgewood NM, US
Paul S. Pickard - Albuquerque NM, US
Milton E. Vernon - Albuquerque NM, US
Fred Gelbard - Albuquerque NM, US
Roger X. Lenard - Edgewood NM, US

Sandia Corporation - Albuquerque NM

B01J 19/00, C01B 17/48

423539, 422129, 422198, 422200, 422201, 422202, 422205

A method and apparatus, constructed of ceramics and other corrosion resistant materials, for decomposing sulfuric acid into sulfur dioxide, oxygen and water using an integrated boiler, superheater, and decomposer unit comprising a bayonet-type, dual-tube, counter-flow heat exchanger with a catalytic insert and a central baffle to increase recuperation efficiency.

2010007, Mar 25, 2010

Sep 24, 2009

12/566595

Roger Xavier Lenard - Edgewood NM, US

Heliosat, Inc. - Dallas TX

B64G 1/00

2441582

A system includes a gravity gradient stabilized space tether. The gravity gradient stabilized space tether includes a tether body having an upper end and a lower end. The gravity gradient stabilized space tether also includes an upper base station located at the upper end of the tether body and a lower base station located at the lower end of the tether body. The gravity gradient stabilized space tether further includes a device coupled to the lower base station. The device can be lowered to a distance below the lower base station to a rendezvous point that is proximate to an orbital path of a sub-orbital vehicle.

7461818, Dec 9, 2008

Feb 7, 2007

11/703296

Robert F. D'Ausilio - Bountiful UT, US
Roger X. Lenard - Edgewood NM, US
James R. Stuart - Louisville CO, US

Iostar Corporation - North Salt Lake UT

B64G 1/40, B64G 1/54

2441711, 2441717

A preferred In Orbit Transportation & Recovery System (IOSTAR™)() includes a space tug powered by a nuclear reactor (). The IOSTAR™ includes a collapsible boom () connected at one end to a propellant tank () which stores fuel for an electric propulsion system (). This end of the boom () is equipped with docking hardware () that is able to grasp and hold a satellite () and as a means to refill the tank (). Radiator panels () mounted on the boom () dissipate heat from the reactor (). A radiation shield () is situated next to the reactor () to protect the satellite payload () at the far end of the boom (). The IOSTAR™ () will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move fully deployed spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.

7484690, Feb 3, 2009

Jan 10, 2007

11/651727

Robert F. D'Ausilio - Bountiful UT, US
James R. Stuart - Louisville CO, US
Roger X. Lenard - Edgewood NM, US

Iostar Corporation - North Salt Lake UT

B64G 1/40, B64G 1/42, B64G 1/64

2441711, 2441717, 2441722

A preferred In Orbit Transportation & Recovery System (IOSTAR™)() includes a space tug powered by a nuclear reactor (). The IOSTAR™ includes a collapsible boom () connected at one end to a propellant tank () which stores fuel for an electric propulsion system (). This end of the boom () is equipped with docking hardware () that is able to grasp and hold a satellite () and as a means to refill the tank (). Radiator panels () mounted on the boom () dissipate heat from the reactor (). A radiation shield () is situated next to the reactor () to protect the satellite payload () at the far end of the boom (). The IOSTAR™ () will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.