Search

Cary Michael Robinson

Examiner (ID: 2649, Phone: (571)270-3316 , Office: P/2923 )

Most Active Art Unit
2923
Art Unit(s)
2954, 2923
Total Applications
1373
Issued Applications
1343
Pending Applications
5
Abandoned Applications
23

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 18029491 [patent_doc_number] => 11512668 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-29 [patent_title] => Multi-pulse solid rocket motor ignition method [patent_app_type] => utility [patent_app_number] => 17/106089 [patent_app_country] => US [patent_app_date] => 2020-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 6568 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17106089 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/106089
Multi-pulse solid rocket motor ignition method Nov 27, 2020 Issued
Array ( [id] => 17330525 [patent_doc_number] => 11220979 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-01-11 [patent_title] => Liquid-cooled air-breathing rocket engine [patent_app_type] => utility [patent_app_number] => 17/094716 [patent_app_country] => US [patent_app_date] => 2020-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 25 [patent_no_of_words] => 8973 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17094716 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/094716
Liquid-cooled air-breathing rocket engine Nov 9, 2020 Issued
Array ( [id] => 17222325 [patent_doc_number] => 11174817 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-11-16 [patent_title] => Air-Breathing rocket engine [patent_app_type] => utility [patent_app_number] => 17/094733 [patent_app_country] => US [patent_app_date] => 2020-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 5446 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17094733 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/094733
Air-Breathing rocket engine Nov 9, 2020 Issued
Array ( [id] => 17579591 [patent_doc_number] => 20220136446 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-05 [patent_title] => TEMPERATURE SENSING FOR TORCH IGNITION SYSTEMS [patent_app_type] => utility [patent_app_number] => 17/089262 [patent_app_country] => US [patent_app_date] => 2020-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6227 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17089262 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/089262
TEMPERATURE SENSING FOR TORCH IGNITION SYSTEMS Nov 3, 2020 Abandoned
Array ( [id] => 17548900 [patent_doc_number] => 20220120241 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-21 [patent_title] => MULTI-PULSE PROPULSION SYSTEM WITH PASSIVE INITIATION [patent_app_type] => utility [patent_app_number] => 17/075987 [patent_app_country] => US [patent_app_date] => 2020-10-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5871 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17075987 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/075987
Multi-pulse propulsion system with passive initiation Oct 20, 2020 Issued
Array ( [id] => 17007914 [patent_doc_number] => 20210239075 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-08-05 [patent_title] => DYNAMIC ROCKET NOZZLE [patent_app_type] => utility [patent_app_number] => 17/075446 [patent_app_country] => US [patent_app_date] => 2020-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2762 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 42 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17075446 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/075446
DYNAMIC ROCKET NOZZLE Oct 19, 2020 Abandoned
Array ( [id] => 19910741 [patent_doc_number] => 12286945 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-04-29 [patent_title] => Hybrid propulsion unit for space vehicle [patent_app_type] => utility [patent_app_number] => 17/769753 [patent_app_country] => US [patent_app_date] => 2020-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 16 [patent_no_of_words] => 1162 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17769753 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/769753
Hybrid propulsion unit for space vehicle Oct 15, 2020 Issued
Array ( [id] => 16808826 [patent_doc_number] => 20210131379 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-05-06 [patent_title] => EXHAUST NOZZLE [patent_app_type] => utility [patent_app_number] => 17/072443 [patent_app_country] => US [patent_app_date] => 2020-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4593 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17072443 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/072443
Exhaust nozzle Oct 15, 2020 Issued
Array ( [id] => 17483057 [patent_doc_number] => 20220090561 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-24 [patent_title] => Motor and Fuel-Powered Hybrid System for a Rocket Thruster [patent_app_type] => utility [patent_app_number] => 16/948516 [patent_app_country] => US [patent_app_date] => 2020-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2354 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16948516 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/948516
Motor and Fuel-Powered Hybrid System for a Rocket Thruster Sep 21, 2020 Abandoned
Array ( [id] => 18071841 [patent_doc_number] => 11530669 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-12-20 [patent_title] => Variable burn-rate solid rocket motor ignition method [patent_app_type] => utility [patent_app_number] => 17/017741 [patent_app_country] => US [patent_app_date] => 2020-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 5600 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17017741 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/017741
Variable burn-rate solid rocket motor ignition method Sep 10, 2020 Issued
Array ( [id] => 16526022 [patent_doc_number] => 20200400102 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-24 [patent_title] => STAGED COMBUSTION LIQUID ROCKET ENGINE CYCLE WITH THE TURBOPUMP UNIT AND PREBURNER INTEGRATED INTO THE STRUCTURE OF THE COMBUSTION CHAMBER [patent_app_type] => utility [patent_app_number] => 17/013457 [patent_app_country] => US [patent_app_date] => 2020-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9804 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 384 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17013457 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/013457
Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber Sep 3, 2020 Issued
Array ( [id] => 19033782 [patent_doc_number] => 20240083597 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-03-14 [patent_title] => Augmented Aerospike Nozzle, Engine Including the Augmented Aerospike Nozzle, and Vehicle Including the Engine [patent_app_type] => utility [patent_app_number] => 17/754787 [patent_app_country] => US [patent_app_date] => 2020-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4463 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 27 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17754787 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/754787
Augmented aerospike nozzle, engine including the augmented aerospike nozzle, and vehicle including the engine Aug 26, 2020 Issued
Array ( [id] => 17399213 [patent_doc_number] => 20220041303 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-02-10 [patent_title] => THRUST WITH THE MINIMUM EJECTION OF PROPELLANT [patent_app_type] => utility [patent_app_number] => 16/985070 [patent_app_country] => US [patent_app_date] => 2020-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2573 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 42 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16985070 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/985070
THRUST WITH THE MINIMUM EJECTION OF PROPELLANT Aug 3, 2020 Abandoned
Array ( [id] => 18871787 [patent_doc_number] => 11859579 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2024-01-02 [patent_title] => System for multiple burns from a rocket motor [patent_app_type] => utility [patent_app_number] => 16/941642 [patent_app_country] => US [patent_app_date] => 2020-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 29 [patent_no_of_words] => 12701 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16941642 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/941642
System for multiple burns from a rocket motor Jul 28, 2020 Issued
Array ( [id] => 19884661 [patent_doc_number] => 12270359 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-04-08 [patent_title] => Tank for containing a component fluid, such as a propellant [patent_app_type] => utility [patent_app_number] => 17/618231 [patent_app_country] => US [patent_app_date] => 2020-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 16 [patent_no_of_words] => 5736 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17618231 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/618231
Tank for containing a component fluid, such as a propellant Jun 8, 2020 Issued
Array ( [id] => 17998405 [patent_doc_number] => 11499505 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-15 [patent_title] => Multi-pulse rocket motor with flight termination destruct charge [patent_app_type] => utility [patent_app_number] => 16/896271 [patent_app_country] => US [patent_app_date] => 2020-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 15 [patent_no_of_words] => 5711 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16896271 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/896271
Multi-pulse rocket motor with flight termination destruct charge Jun 8, 2020 Issued
Array ( [id] => 17997614 [patent_doc_number] => 11498705 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-11-15 [patent_title] => On orbit fluid propellant dispensing systems and methods [patent_app_type] => utility [patent_app_number] => 16/871144 [patent_app_country] => US [patent_app_date] => 2020-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3569 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16871144 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/871144
On orbit fluid propellant dispensing systems and methods May 10, 2020 Issued
Array ( [id] => 17604629 [patent_doc_number] => 11333105 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-05-17 [patent_title] => Thrust chamber liner and fabrication method therefor [patent_app_type] => utility [patent_app_number] => 16/860989 [patent_app_country] => US [patent_app_date] => 2020-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 5079 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16860989 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/860989
Thrust chamber liner and fabrication method therefor Apr 27, 2020 Issued
Array ( [id] => 18838186 [patent_doc_number] => 11846251 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-12-19 [patent_title] => Liquid rocket engine booster engine with combustion gas fuel source [patent_app_type] => utility [patent_app_number] => 16/857609 [patent_app_country] => US [patent_app_date] => 2020-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 14 [patent_no_of_words] => 6609 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16857609 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/857609
Liquid rocket engine booster engine with combustion gas fuel source Apr 23, 2020 Issued
Array ( [id] => 18315595 [patent_doc_number] => 11629669 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-04-18 [patent_title] => Liquid monopropellant controlled solid rocket motor with aft end injection deflector [patent_app_type] => utility [patent_app_number] => 16/831025 [patent_app_country] => US [patent_app_date] => 2020-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 12 [patent_no_of_words] => 6383 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16831025 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/831025
Liquid monopropellant controlled solid rocket motor with aft end injection deflector Mar 25, 2020 Issued
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