Patent Assignment
Reel/Frame 030311/0327
Security Agreement
Recorded: 2013-04-29
Received: 2013-04-29
Pages: 16
Assignor
SPACE SYSTEMS/LORAL, LLC
Executed: 2012-11-02
Assignee
ROYAL BANK OF CANADA
200 BAY STREET, P.O. BOX 1, ROYAL BANK PLAZA, TORONTO, ON, CAX, M5J 2J5, CANADA
Covered Properties
(37)
Moisture Curable Silylated Polymer Compositions Containing Reactive Modifiers
Application:
13/608,142 →
Ground-Based Beamforming for Satellite Communications Systems
Application:
12/856,468 →
Image Navigation Method Using Parametric Systematic Error Correction
Application:
12/800,450 →
Antenna Tracking Profile Estimation
Application:
12/779,872 →
Satellite System with Enhanced Payload Capacity
Application:
12/344,064 →
Redundant Radial Release Apparatus
Application:
12/215,041 →
Multi-Beam Satellite Network to Maximize Bandwidth Utilization
Application:
11/891,086 →
Spacecraft Three-Axis Attitude Acquisition from Sun Direction Measurement
Application:
11/709,614 →
Ground-Based Beamforming for Satellite Communications Systems
Application:
11/467,490 →
Sealant Composition Having Reduced Permeability to Gas
Application:
11/345,563 →
Antenna Distortion Estimation and Compensation
Application:
10/244,944 →
Single-Receiver Multiple-Antenna Rf Autotrack Control
Application:
10/097,678 →
Cdma Code Address Data Routing System and Method
Application:
10/094,898 →
Satellite Harmonic Torque Estimator
Application:
10/087,279 →
Spacecraft Having a Momentum Wheel Configuration That Prevents Zero Wheel Speeds
Application:
09/995,017 →
Multi-Band Corrugated Antenna Feed Horn with a Hexagonal Aperture and Antenna Array Using Same
Application:
10/002,808 →
Two-Sided Deployable Thermal Radiator System and Method
Application:
10/007,256 →
Passive Intermodulation Free Multilayer Thermal Blanket
Application:
10/020,704 →
Hybrid Horn for Dual Ka-Band Communications
Application:
10/036,347 →
Energy Managed Electric Propulsion Methods and Systems for Stationkeeping Satellites
Application:
09/977,834 →
Dielectric Resonator Equalizer
Application:
09/957,734 →
Electric Orbit Raising with Variable Thrust
Application:
09/947,186 →
Spacecraft Constellation Formation Keeping Using Inter-Spacecraft Distance Measurement
Application:
09/931,205 →
Methods for Testing Multibeam Satellite Systems Using Input Power Telemetry and Output Noise Power
Application:
09/912,167 →
Method and System for Synchronized Forward and Aft Thrust Vector Control
Application:
09/883,622 →
Method and Apparatus for Soft Switched Ac Power Distribution
Application:
09/884,734 →
Phase Change Material Thermal Control for Electric Propulsion
Application:
09/881,942 →
Voltage Tunable Patch Filter Element with Dielectrically Loaded Slot
Application:
09/880,381 →
Satellite Communication System with Gateway Switch Networks
Application:
09/871,075 →
Multiple Passband Filter
Application:
09/850,695 →
Spacecraft Radiator System and Method Using Cross-Coupled Deployable Thermal Radiators
Application:
09/841,373 →
Waveguide Slot Array Capable of Radiating Shaped Beams
Application:
09/835,795 →
Heat Transfer of a Remote Heat Source Using a Loop Heat Pipe
Application:
09/822,073 →
Dynamic Resource Allocation Architecture for Differentiated Services Over Broadband Communication Networks
Application:
09/822,691 →
Flexible Waveguide with Rounded Corrugations
Application:
09/818,489 →
Triple Reflector Antenna Deployment and Storage Systems
Application:
09/812,298 →
Noise Screen for Attitude Control System
Application:
09/782,644 →