
Lissi Mojica Marquis
Examiner (ID: 12147)
| Most Active Art Unit | 3104 |
| Art Unit(s) | 3614, 3661, 3104, 3105, 3107, 3613 |
| Total Applications | 667 |
| Issued Applications | 565 |
| Pending Applications | 34 |
| Abandoned Applications | 68 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2963795
[patent_doc_number] => 05251855
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-12
[patent_title] => 'Spacecraft propulsion system thruster firing system'
[patent_app_type] => 1
[patent_app_number] => 7/995520
[patent_app_country] => US
[patent_app_date] => 1992-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1643
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/251/05251855.pdf
[firstpage_image] =>[orig_patent_app_number] => 995520
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/995520 | Spacecraft propulsion system thruster firing system | Dec 21, 1992 | Issued |
Array
(
[id] => 3075439
[patent_doc_number] => 05284309
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-02-08
[patent_title] => 'Propellant immobilizing system and method'
[patent_app_type] => 1
[patent_app_number] => 7/992397
[patent_app_country] => US
[patent_app_date] => 1992-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2271
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 235
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/284/05284309.pdf
[firstpage_image] =>[orig_patent_app_number] => 992397
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/992397 | Propellant immobilizing system and method | Dec 17, 1992 | Issued |
Array
(
[id] => 3408936
[patent_doc_number] => 05452869
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-09-26
[patent_title] => 'On-board three-axes attitude determination and control system'
[patent_app_type] => 1
[patent_app_number] => 7/993948
[patent_app_country] => US
[patent_app_date] => 1992-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 34
[patent_no_of_words] => 15917
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/452/05452869.pdf
[firstpage_image] =>[orig_patent_app_number] => 993948
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/993948 | On-board three-axes attitude determination and control system | Dec 17, 1992 | Issued |
Array
(
[id] => 3468797
[patent_doc_number] => 05398890
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-03-21
[patent_title] => 'Pneumatic deicer assembly having a self connecting shell'
[patent_app_type] => 1
[patent_app_number] => 7/981672
[patent_app_country] => US
[patent_app_date] => 1992-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 2674
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/398/05398890.pdf
[firstpage_image] =>[orig_patent_app_number] => 981672
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/981672 | Pneumatic deicer assembly having a self connecting shell | Nov 24, 1992 | Issued |
| 07/981159 | SPLIT AIRFOIL AERODYNAMICALLY CONFIGURED TO FACILITATE CLOSURE | Nov 23, 1992 | Abandoned |
Array
(
[id] => 3025017
[patent_doc_number] => 05372340
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-12-13
[patent_title] => 'Spacecraft system'
[patent_app_type] => 1
[patent_app_number] => 7/972766
[patent_app_country] => US
[patent_app_date] => 1992-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 30
[patent_no_of_words] => 6162
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/372/05372340.pdf
[firstpage_image] =>[orig_patent_app_number] => 972766
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/972766 | Spacecraft system | Nov 4, 1992 | Issued |
Array
(
[id] => 2947549
[patent_doc_number] => 05273237
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-12-28
[patent_title] => 'Forebody nozzle for aircraft directional control'
[patent_app_type] => 1
[patent_app_number] => 7/970747
[patent_app_country] => US
[patent_app_date] => 1992-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 1868
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 204
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/273/05273237.pdf
[firstpage_image] =>[orig_patent_app_number] => 970747
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/970747 | Forebody nozzle for aircraft directional control | Nov 1, 1992 | Issued |
Array
(
[id] => 3043355
[patent_doc_number] => 05337978
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-16
[patent_title] => 'Leading edge pneumatic deicer assembly'
[patent_app_type] => 1
[patent_app_number] => 7/968118
[patent_app_country] => US
[patent_app_date] => 1992-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 3962
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/337/05337978.pdf
[firstpage_image] =>[orig_patent_app_number] => 968118
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/968118 | Leading edge pneumatic deicer assembly | Oct 28, 1992 | Issued |
Array
(
[id] => 2961107
[patent_doc_number] => 05255873
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-26
[patent_title] => 'Flying wing space launch assist stage'
[patent_app_type] => 1
[patent_app_number] => 7/962966
[patent_app_country] => US
[patent_app_date] => 1992-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 2112
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/255/05255873.pdf
[firstpage_image] =>[orig_patent_app_number] => 962966
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/962966 | Flying wing space launch assist stage | Oct 18, 1992 | Issued |
Array
(
[id] => 3056252
[patent_doc_number] => 05335880
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-09
[patent_title] => 'Cargo compartment door for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/962147
[patent_app_country] => US
[patent_app_date] => 1992-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2997
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/335/05335880.pdf
[firstpage_image] =>[orig_patent_app_number] => 962147
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/962147 | Cargo compartment door for an aircraft | Oct 15, 1992 | Issued |
Array
(
[id] => 3001336
[patent_doc_number] => 05340060
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-23
[patent_title] => 'Rendezvous docking optical sensor system'
[patent_app_type] => 1
[patent_app_number] => 7/957706
[patent_app_country] => US
[patent_app_date] => 1992-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 4079
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/340/05340060.pdf
[firstpage_image] =>[orig_patent_app_number] => 957706
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/957706 | Rendezvous docking optical sensor system | Oct 6, 1992 | Issued |
Array
(
[id] => 2916681
[patent_doc_number] => 05232184
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-03
[patent_title] => 'Self-staging parachute apparatus'
[patent_app_type] => 1
[patent_app_number] => 7/949936
[patent_app_country] => US
[patent_app_date] => 1992-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 14
[patent_no_of_words] => 3545
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 503
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/232/05232184.pdf
[firstpage_image] =>[orig_patent_app_number] => 949936
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/949936 | Self-staging parachute apparatus | Sep 23, 1992 | Issued |
| 07/949110 | SPACECRAFT BERTHING MECHANISM | Sep 22, 1992 | Abandoned |
Array
(
[id] => 2983572
[patent_doc_number] => 05358199
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-10-25
[patent_title] => 'Automatic flight control system having unified graphic mistrim indicator'
[patent_app_type] => 1
[patent_app_number] => 7/947026
[patent_app_country] => US
[patent_app_date] => 1992-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 6
[patent_no_of_words] => 2049
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/358/05358199.pdf
[firstpage_image] =>[orig_patent_app_number] => 947026
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/947026 | Automatic flight control system having unified graphic mistrim indicator | Sep 16, 1992 | Issued |
Array
(
[id] => 3082730
[patent_doc_number] => 05318250
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-06-07
[patent_title] => 'Pilot visual assurance apparatus for an aircraft cockpit'
[patent_app_type] => 1
[patent_app_number] => 7/943828
[patent_app_country] => US
[patent_app_date] => 1992-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 19
[patent_no_of_words] => 3665
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/318/05318250.pdf
[firstpage_image] =>[orig_patent_app_number] => 943828
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/943828 | Pilot visual assurance apparatus for an aircraft cockpit | Sep 10, 1992 | Issued |
Array
(
[id] => 2963777
[patent_doc_number] => 05251854
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-12
[patent_title] => 'Two-sailed sport kite'
[patent_app_type] => 1
[patent_app_number] => 7/940307
[patent_app_country] => US
[patent_app_date] => 1992-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 18
[patent_no_of_words] => 2807
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/251/05251854.pdf
[firstpage_image] =>[orig_patent_app_number] => 940307
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/940307 | Two-sailed sport kite | Sep 2, 1992 | Issued |
Array
(
[id] => 3470153
[patent_doc_number] => 05405108
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-04-11
[patent_title] => 'Space debris clearing device'
[patent_app_type] => 1
[patent_app_number] => 7/940147
[patent_app_country] => US
[patent_app_date] => 1992-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2795
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/405/05405108.pdf
[firstpage_image] =>[orig_patent_app_number] => 940147
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/940147 | Space debris clearing device | Sep 2, 1992 | Issued |
Array
(
[id] => 2929046
[patent_doc_number] => 05253824
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-19
[patent_title] => 'Hollow core airfoil'
[patent_app_type] => 1
[patent_app_number] => 7/939531
[patent_app_country] => US
[patent_app_date] => 1992-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 1959
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/253/05253824.pdf
[firstpage_image] =>[orig_patent_app_number] => 939531
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/939531 | Hollow core airfoil | Aug 31, 1992 | Issued |
Array
(
[id] => 3495664
[patent_doc_number] => 05568904
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-10-29
[patent_title] => 'Steered perigee velocity augmentation'
[patent_app_type] => 1
[patent_app_number] => 7/937957
[patent_app_country] => US
[patent_app_date] => 1992-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1547
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/568/05568904.pdf
[firstpage_image] =>[orig_patent_app_number] => 937957
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/937957 | Steered perigee velocity augmentation | Aug 27, 1992 | Issued |
Array
(
[id] => 2903898
[patent_doc_number] => 05205517
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-27
[patent_title] => 'Large parachute with means to positively expand and circularize the inlet area to facilitate deployment thereof'
[patent_app_type] => 1
[patent_app_number] => 7/936166
[patent_app_country] => US
[patent_app_date] => 1992-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 16
[patent_no_of_words] => 3295
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 375
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/205/05205517.pdf
[firstpage_image] =>[orig_patent_app_number] => 936166
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/936166 | Large parachute with means to positively expand and circularize the inlet area to facilitate deployment thereof | Aug 26, 1992 | Issued |