Patent Assignment
Reel/Frame 074270/0351
CHANGE OF NAME
Recorded: 2026-01-07
Received: 2026-01-07
Pages: 9
Assignor
MAXAR SPACE LLC
Executed: 2025-10-01
Assignee
LANTERIS SPACE LLC
3825 FABIAN WAY, PALO ALTO, CA, 94303, UNITED STATES
Covered Applications
(100)
PASSIVELY DAMPED END FITTINGS AND BRACKETS
App. No. 18/970,457
→
SEALING OF MULTI-LAYER INSULATION BLANKETS FOR SPACECRAFT
App. No. 18/620,445
→
MODULAR SOLAR ARRAY
App. No. 18/501,264
→
DISPENSING HINGE ASSEMBLY
App. No. 18/353,548
→
LINKED SPACECRAFT DISPENSING
App. No. 18/353,534
→
ANTENNA REFLECTOR SPACECRAFT TEMPERATURE REGULATION DURING ORBIT RAISING
App. No. 18/305,190
→
SOLAR ARRAY SPRING ELEMENTS FOR STACKING SPACECRAFT
App. No. 18/304,249
→
STACKED SPACECRAFT LAUNCH AND ORBIT RAISING
App. No. 18/302,754
→
CONTINUOUS ROTATION ROVER SUSPENSION WITH CONSTANT VERTICAL STEERING AXIS
App. No. 18/116,106
→
SATELLITE PROPELLANT TANK WITH INTEGRATED REGULATION
App. No. 17/991,671
→
CONNECTOR LOADING DEVICE
App. No. 18/054,747
→
PASSIVE THERMAL RADIATOR STRUCTURE
App. No. 17/979,579
→
SHOCKLESS SPACECRAFT DISPENSER
App. No. 17/967,582
→
SPACECRAFT PROPULSION AND POSITIONER SIMULATOR
App. No. 17/966,470
→
MULTI-SPACECRAFT DEPLOYMENT
App. No. 17/952,050
→
MODULAR SOLAR ARRAY
App. No. 17/948,011
→
THERMALLY EFFICIENT BUS HOUSING
App. No. 17/939,290
→
Z-FOLD SOLAR ARRAY WITH CURVED SUBSTRATE PANELS
App. No. 17/886,152
→
MANEUVERING OF SATELLITES WITHOUT RATE SENSORS
App. No. 17/850,164
→
MODULAR ARCHITECTURE AVIONICS
App. No. 17/835,866
→
SOLAR ARRAY REVERSE CURRENT PROTECTION
App. No. 17/748,970
→
MICROCONTROLLER BASED SOLAR ARRAY ENERGY TRANSFER BATTERY CHARGE CONTROL
App. No. 17/744,437
→
SPACECRAFT THRUSTER VOLTAGE MEASUREMENT UNIT
App. No. 17/742,840
→
POWER PROCESSING UNIT (PPU) AND ELECTRIC PROPULSION SYSTEM (EPS) FOR SPACECRAFT
App. No. 17/737,432
→
3D PRINTED SPACECRAFT STRUCTURES
App. No. 17/714,939
→
SPACECRAFT PROPELLANT LOADING SYSTEM
App. No. 17/714,845
→
ANTENNA WITH MOVABLE FEED
App. No. 17/714,067
→
SATELLITE BOOM END EFFECTOR
App. No. 17/707,475
→
CONVOLUTIONAL NEURAL NETWORK (CNN) FOR AUTOMATIC TARGET RECOGNITION IN A SATELLITE
App. No. 17/696,709
→
DETERMINATION OF A CONVOLUTIONAL NEURAL NETWORK (CNN) FOR AUTOMATIC TARGET RECOGNITION IN A RESOURCE CONSTRAINED ENVIRONMENT
App. No. 17/696,707
→
SEALING OF MULTI-LAYER INSULATION BLANKETS FOR SPACECRAFT
App. No. 17/694,534
→
SATELLITE WITH MODULAR RADIATOR PANELS
App. No. 17/580,966
→
DISPENSERLESS MULTI-SATELLITE LAUNCH CONFIGURATION WITH SIMPLE ADAPTER INTERFACE
App. No. 17/554,000
→
FOLD-OUT SATELLITE WITH INTEGRATED RADIATOR PANEL
App. No. 17/538,161
→
HIGH LINEARITY SATELLITE PAYLOAD USING SOLID STATE POWER AMPLIFIERS
App. No. 17/509,579
→
RETRACTABLE Z-FOLD FLEXIBLE BLANKET SOLAR ARRAY
App. No. 17/505,359
→
SMALL SATELLITE CONSTELLATION FOR WORLDWIDE SURVEILLANCE
App. No. 17/478,531
→
PARTIALLY FLEXIBLE SOLAR ARRAY STRUCTURE
App. No. 17/463,670
→
MULTI-SATELLITE DEPLOYABLE DISPENSER
App. No. 17/410,702
→
STACKABLE SATELLITE DISPENSING CONFIGURATION
App. No. 17/410,433
→
Z-FOLD FLEXIBLE BLANKET SOLAR ARRAY
App. No. 17/398,319
→
ADDITIVE MANUFACTURING ON-ORBIT
App. No. 17/234,664
→
FLEXIBLE BANDWIDTH ASSIGNMENT TO SPOT BEAMS
App. No. 17/204,033
→
METHOD OF OPERATING A SPACECRAFT RADIATOR PANEL
App. No. 17/180,615
→
PASSIVELY DAMPED END FITTINGS AND BRACKETS
App. No. 17/124,696
→
AGGREGATED SPACE SYSTEM NETWORK
App. No. 17/110,127
→
MULTI-MISSION CONFIGURABLE SPACECRAFT SYSTEM
App. No. 17/110,115
→
FLEXIBLE MICROMETEOROID SHIELD
App. No. 17/089,610
→
SPACECRAFT WITH UNIVERSAL TEST PORT
App. No. 17/083,004
→
DAYSIDE-ONLY ROLL STEERING
App. No. 17/076,444
→
SYSTEMS AND METHODS FOR SATELLITE MOVEMENT
App. No. 17/038,213
→
SPACECRAFT WITH UNIVERSAL EXTERNAL PORT
App. No. 17/022,550
→
STRUCTURAL ARRANGEMENTS USING CARBON FIBER BRAID
App. No. 16/855,483
→
DEPLOYMENT MECHANISM WITH INTEGRAL ACTUATION DEVICE
App. No. 16/817,286
→
SPACECRAFT DESIGN WITH SEMI-RIGID SOLAR ARRAY
App. No. 16/813,559
→
SMALLSAT PAYLOAD CONFIGURATION
App. No. 16/748,617
→
HIGH LINEARITY SATELLITE PAYLOAD USING SOLID STATE POWER AMPLIFIERS
App. No. 16/683,520
→
SPACECRAFT EXOSKELETON TRUSS STRUCTURE
App. No. 16/539,348
→
SATELLITE DIVERSITY
App. No. 16/505,937
→
HIGH AVAILABILITY SCALABLE MULTI-SOURCE VIRTUALIZED SPECTRUM SIGNAL PROCESSING SYSTEM
App. No. 16/434,481
→
MULTIPORT AMPLIFIER INPUT NETWORK WITH COMPENSATION FOR OUTPUT NETWORK GAIN AND PHASE FREQUENCY RESPONSE IMBALANCE
App. No. 16/405,162
→
GROUND BASED SUBSYSTEMS, FOR INCLUSION IN OPTICAL GATEWAY, AND THAT INTERFACE WITH OPTICAL NETWORKS EXTERNAL TO OPTICAL GATEWAY
App. No. 16/168,658
→
FLEXIBLE BANDWIDTH ASSIGNMENT TO SPOT BEAMS
App. No. 16/163,105
→
HIGH LINEARITY SATELLITE PAYLOAD USING SOLID STATE POWER AMPLIFIERS
App. No. 16/113,567
→
SATELLITE SYSTEM USING AN RF GBBF FEEDER UPLINK BEAM FROM A GATEWAY TO A SATELLITE, AND USING AN OPTICAL ISL FROM THE SATELLITE TO ANOTHER SATELLITE
App. No. 16/111,008
→
SPACECRAFT PROPELLANT MANAGEMENT SYSTEM
App. No. 15/985,357
→
UNIFIED SPACECRAFT PROPELLANT MANAGEMENT SYSTEM FOR CHEMICAL AND ELECTRIC PROPULSION
App. No. 15/970,693
→
MULTIPORT AMPLIFIER INPUT NETWORK WITH COMPENSATION FOR OUTPUT NETWORK GAIN AND PHASE FREQUENCY RESPONSE IMBALANCE
App. No. 15/926,186
→
SATELLITE SYSTEM CALIBRATION IN ACTIVE OPERATIONAL CHANNELS
App. No. 15/926,628
→
MULTIPLE THRUSTER FIRING ON A SINGLE ARTICULABLE MODULE
App. No. 15/920,294
→
FLEXIBLE SIGNAL DISTRIBUTION ASSISTED BY TUNABLE OPTICAL CARRIER MODULATING A DESIRED SIGNAL
App. No. 15/904,063
→
LOW EARTH ORBITING SPACECRAFT WITH A DUAL-USE DIRECTIONAL ANTENNA
App. No. 15/900,653
→
HIGH CAPACITY COMMUNICATION SATELLITE
App. No. 15/887,721
→
ADDITIVE MANUFACTURING ON-ORBIT
App. No. 15/885,484
→
SPACECRAFT WITH AERODYNAMIC CONTROL
App. No. 15/849,289
→
ON-ORBIT ASSEMBLY OF COMMUNICATION SATELLITES
App. No. 15/847,780
→
CALIBRATION OF SATELLITE BEAMFORMING CHANNELS
App. No. 15/833,351
→
POINTING SYSTEM IMPROVEMENT WITH IMAGING ARRAY FEEDS
App. No. 15/831,257
→
MODULARIZED FEED ARRAY ARRANGEMENT
App. No. 15/831,258
→
LAMINATE SANDWICH PANEL
App. No. 15/818,539
→
ADDITIVE MANUFACTURED RF MODULE
App. No. 15/818,542
→
ON-ORBIT PROPELLANT METERING AND REFUELING
App. No. 15/809,856
→
SATELLITE WITH REGENERATIVE PROCESSOR
App. No. 15/799,258
→
SPACECRAFT RENDEZVOUS AND DOCKING TECHNIQUES
App. No. 15/729,502
→
ADAPTIVE COMMUNICATION SYSTEM
App. No. 15/710,740
→
HIGH POINTING ACCURACY SPACECRAFT
App. No. 15/709,341
→
AMPLIFIER INTEGRATED FEED ARRAY WITH MODULARIZED FEED ELEMENTS AND AMPLIFIERS
App. No. 15/699,909
→
SELF-ASSEMBLING PERSISTENT SPACE PLATFORM
App. No. 15/689,993
→
SATELLITE SYSTEM USING OPTICAL GATEWAYS AND GROUND BASED BEAMFORMING
App. No. 15/682,785
→
RECONFIGURABLE SPACECRAFT WITH A HOLD-DOWN ASSEMBLY FOR A RIGID REFLECTOR
App. No. 15/669,470
→
POWER TRAIN FOR DEEP SPACE SOLAR ELECTRIC PROPULSION
App. No. 15/659,395
→
SPACE BASED ROBOTIC ASSEMBLY OF A MODULAR REFLECTOR
App. No. 15/654,593
→
FLEXIBLE HIGH THROUGHPUT SATELLITE SYSTEM USING OPTICAL GATEWAYS
App. No. 15/633,007
→
METHOD AND APPARATUS FOR CALIBRATION AND EQUALIZATION OF MULTIPORT AMPLIFIERS (MPAs)
App. No. 15/628,140
→
LATTICE STRUCTURE DESIGN AND MANUFACTURING TECHNIQUES
App. No. 15/622,888
→
SATELLITE NETWORK SWITCHING
App. No. 15/618,897
→
CROSS-FEEDING PROPELLANT BETWEEN STACKED SPACECRAFT
App. No. 15/616,803
→
COMMUNICATION PLATFORM WITH FLEXIBLE PHOTONICS PAYLOAD
App. No. 15/604,165
→
ECLIPTIC SUN ACQUISITION CONTROL MODE FOR SATELLITES
App. No. 15/603,288
→
SATELLITE SYSTEM USING OPTICAL GATEWAYS AND ONBOARD PROCESSING
App. No. 15/599,852
→