Galen L. Barefoot

Array ( [id] => 6028495 [patent_doc_number] => 20020017591 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-02-14 [patent_title] => 'Drive unit for a model helicopter' [patent_app_type] => new [patent_app_number] => 09/860527 [patent_app_country] => US [patent_app_date] => 2001-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2242 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 25 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0017/20020017591.pdf [firstpage_image] =>[orig_patent_app_number] => 09860527 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1437804 [patent_doc_number] => 06494402 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-12-17 [patent_title] => 'Lateral exhaust microthruster' [patent_app_type] => B2 [patent_app_number] => 09/855005 [patent_app_country] => US [patent_app_date] => 2001-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2210 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/494/06494402.pdf [firstpage_image] =>[orig_patent_app_number] => 09855005 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1400957 [patent_doc_number] => 06511016 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-01-28 [patent_title] => 'Spin-stabilized projectile with a braking device' [patent_app_type] => B2 [patent_app_number] => 09/853107 [patent_app_country] => US [patent_app_date] => 2001-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3305 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 240 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/511/06511016.pdf [firstpage_image] =>[orig_patent_app_number] => 09853107 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1318553 [patent_doc_number] => 06598831 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-07-29 [patent_title] => 'Device suspended to a carrier for rescuing people or equipment' [patent_app_type] => B1 [patent_app_number] => 09/762314 [patent_app_country] => US [patent_app_date] => 2001-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2815 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/598/06598831.pdf [firstpage_image] =>[orig_patent_app_number] => 09762314 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6348347 [patent_doc_number] => 20020056790 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-05-16 [patent_title] => 'Micro louvers for cooling satellites' [patent_app_type] => new [patent_app_number] => 09/841483 [patent_app_country] => US [patent_app_date] => 2001-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2415 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 50 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0056/20020056790.pdf [firstpage_image] =>[orig_patent_app_number] => 09841483 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6122998 [patent_doc_number] => 20020074459 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-06-20 [patent_title] => 'Pressure control system for a pressure-expandable displacement element' [patent_app_type] => new [patent_app_number] => 09/837637 [patent_app_country] => US [patent_app_date] => 2001-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 6885 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 314 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0074/20020074459.pdf [firstpage_image] =>[orig_patent_app_number] => 09837637 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1554269 [patent_doc_number] => 06435097 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-20 [patent_title] => 'Protective device for deployable fins of artillery projectiles' [patent_app_type] => B1 [patent_app_number] => 09/828441 [patent_app_country] => US [patent_app_date] => 2001-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1938 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/435/06435097.pdf [firstpage_image] =>[orig_patent_app_number] => 09828441 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1574279 [patent_doc_number] => 06446906 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-10 [patent_title] => 'Fin and cover release system' [patent_app_type] => B1 [patent_app_number] => 09/825808 [patent_app_country] => US [patent_app_date] => 2001-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 2883 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 251 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/446/06446906.pdf [firstpage_image] =>[orig_patent_app_number] => 09825808 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1499437 [patent_doc_number] => 06464165 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-15 [patent_title] => 'Image display craft' [patent_app_type] => B1 [patent_app_number] => 09/701816 [patent_app_country] => US [patent_app_date] => 2001-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 4 [patent_no_of_words] => 1157 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/464/06464165.pdf [firstpage_image] =>[orig_patent_app_number] => 09701816 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6885541 [patent_doc_number] => 20010018810 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-09-06 [patent_title] => 'Spacecraft advertisement method and system' [patent_app_type] => new [patent_app_number] => 09/811539 [patent_app_country] => US [patent_app_date] => 2001-03-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2398 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0018/20010018810.pdf [firstpage_image] =>[orig_patent_app_number] => 09811539 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5840029 [patent_doc_number] => 20020130220 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-09-19 [patent_title] => 'Airships having simplied construction and improved maneuverability' [patent_app_type] => new [patent_app_number] => 09/730870 [patent_app_country] => US [patent_app_date] => 2001-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3470 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0130/20020130220.pdf [firstpage_image] =>[orig_patent_app_number] => 09730870 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1394335 [patent_doc_number] => 06548794 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-04-15 [patent_title] => 'Dissolvable thrust vector control vane' [patent_app_type] => B2 [patent_app_number] => 09/804897 [patent_app_country] => US [patent_app_date] => 2001-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 5653 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/548/06548794.pdf [firstpage_image] =>[orig_patent_app_number] => 09804897 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 787244 [patent_doc_number] => 06986486 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-01-17 [patent_title] => 'Aircraft control system' [patent_app_type] => utility [patent_app_number] => 10/240190 [patent_app_country] => US [patent_app_date] => 2001-03-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2365 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/986/06986486.pdf [firstpage_image] =>[orig_patent_app_number] => 10240190 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6413829 [patent_doc_number] => 20020125371 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-09-12 [patent_title] => 'AIRCRAFT AND AIRCRAFT MANUFACTURING METHOD' [patent_app_type] => new [patent_app_number] => 09/801308 [patent_app_country] => US [patent_app_date] => 2001-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2251 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0125/20020125371.pdf [firstpage_image] =>[orig_patent_app_number] => 09801308 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6885819 [patent_doc_number] => 20010019088 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-09-06 [patent_title] => 'Wing-drive mechanism and vehicle employing same' [patent_app_type] => new [patent_app_number] => 09/793333 [patent_app_country] => US [patent_app_date] => 2001-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 18011 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0019/20010019088.pdf [firstpage_image] =>[orig_patent_app_number] => 09793333 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1558078 [patent_doc_number] => 06360994 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-03-26 [patent_title] => 'Configurable space launch system' [patent_app_type] => B1 [patent_app_number] => 09/792740 [patent_app_country] => US [patent_app_date] => 2001-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 7821 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/360/06360994.pdf [firstpage_image] =>[orig_patent_app_number] => 09792740 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1311905 [patent_doc_number] => 06604706 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-08-12 [patent_title] => 'Gyrostabilized self propelled aircraft' [patent_app_type] => B1 [patent_app_number] => 09/763714 [patent_app_country] => US [patent_app_date] => 2001-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 23 [patent_no_of_words] => 9317 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 211 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/604/06604706.pdf [firstpage_image] =>[orig_patent_app_number] => 09763714 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1371466 [patent_doc_number] => 06543721 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-04-08 [patent_title] => 'Stressed-skin component made of metal' [patent_app_type] => B2 [patent_app_number] => 09/774091 [patent_app_country] => US [patent_app_date] => 2001-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2309 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/543/06543721.pdf [firstpage_image] =>[orig_patent_app_number] => 09774091 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6012107 [patent_doc_number] => 20020100836 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-01 [patent_title] => 'Hydrogen and oxygen battery, or hudrogen and oxygen to fire a combustion engine and/or for commerce.' [patent_app_type] => new [patent_app_number] => 09/774110 [patent_app_country] => US [patent_app_date] => 2001-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 29 [patent_no_of_words] => 22434 [patent_no_of_claims] => 143 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 31 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0100/20020100836.pdf [firstpage_image] =>[orig_patent_app_number] => 09774110 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1329519 [patent_doc_number] => 06588708 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-07-08 [patent_title] => 'Spacecraft methods and structures for acquiring and determining power-safe attitudes' [patent_app_type] => B2 [patent_app_number] => 09/771916 [patent_app_country] => US [patent_app_date] => 2001-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 14 [patent_no_of_words] => 5952 [patent_no_of_claims] => 35 [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/06/588/06588708.pdf [firstpage_image] =>[orig_patent_app_number] => 09771916 [rel_patent_id] =>[rel_patent_doc_number] =>)