Спутник технологический. STP-R1. [Редактировать]

Экспериментальный демонстратор технологий для DARPA с целью продемонстрировать «быструю реакцию» на приказ о запуске.

Дополнительные наименования

#НаименованияПоиск в новостяхПоиск в документах
1StreakНайтиНайти
2USA 185НайтиНайти
328871НайтиНайти

Дополнительная классификация

#Наименования
1Тип оператора(владельца) - военные
2Страна оператор(владелец) - США
3Страна производитель - США

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг417

Характеристики орбиты

#ХарактеристикаЗначение
1Дата (сведения с орбиты)2006-06-28

Пусковые характеристики

#ХарактеристикаЗначение
1Код NSSDC2005-037A

Информация об удачном запуске

#ХарактеристикаЗначение
1Дата пуска2005-09-23 at 02:24:00 UTC
2Полезная нагрузка 1xSTP-R1
3Ракета-носитель 1xМинотавр 1

Найдено 528 документов по запросу «STP-R1». [Перейти к поиску]


Дата загрузки: 2017-04-08
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0.09/5
... Force payloads XSS-11 and STP R1 in April and September, respectively... 181, USA 182, USA 186, STP R1, and XSS-11); Of the... successful. • Seven Russian payloads (Glonass K R1, Glonass K R2, Glonass K R3, Kosmos... of military navigation satellites, Glonass K R1-R3. Russia also performed three... GEO Telesat Canada Astrium Communications S S STP R1 LEO USAF USAF Research Laboratory... NPO Prikladnoy Mekhaniki Communications S S Glonass K R1 MEO Russian MoD NPO Prikladnoy...



Дата загрузки: 2017-03-10
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0.08/5
... 2005, while a second Minotaur I launched STP-R1 in support of the Defense... Flight mission (July–August 2005), STP managed crew training, the on... F i s c a l The DOD Space Test Program (STP), Rocket Systems Launch Program 23... Air Force, US Navy, and STP, provided the remaining 20 percent...) Interplanetary probe Sept. 23, 2005 STP-R1 2005-037A OSC Minotaur Technology... Authorization Space Telescope Imaging Spectrograph STP SURF SVS Space Test Program...



Дата загрузки: 2017-01-04
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0.31/5
... Un dt 2 d 2 U1 dt 2 + Fтр1 + r1 + Fтрi + ri dUi + k i (2Ui − Ui... q TP τ q β θ τ p O1 l1 n q n p Rp lp r1 r2 ϕ2 ,Φ2 O2 T1 Рис. 1 Уравнения... механизм станка СТБ. На рис. 1: r1 – радиус скала; r2 – длина коромысла... механизма описывается следующими дифференциальными уравнениями: && 2 = STP r1 + r2 ( N − N J2ϕ τ q τ p ) − m gr cos ϕ 1 2 2 Умножим... 1 + J1 M, J 2 − J1 (5) & = M, (J 2 − J1 )Φ 2 &&1 , + R p l p sin θ − J1ϕ &&1 = STP − J1ϕ && 2 . J1ϕ (4) Здесь Sтр – суммарная... следующие конструктивные размеры станка СТБ: r1=0,075 м; r2=0,152 м; fтр=0,3; ρ=800... α от α 0 на величину ϕ . Так как R1 и R 2 соответствуют участкам тросов: Ri ≈ R i0... Δ i ≤ 0 или R i0 ≤ 0, R i0 ≈ ci Δ i + bi Δ& i , εi , i = 1, 2 , Δ1 = − r1β − rкϕ , Δ 2 = r2β − yг , 140 t =0 , где... и коэффициент демпфирования элементов 6 и 7 (см. рис. 1); h R1 = rк ; h P = l cos ( α 0 + ϕ + λ ) ; l – расстояние OC (см...



Дата загрузки: 2017-04-24
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0.06/5
... Titan 405B Imaging LEO US STP-R1 Minotaur Technology LEO US Navstar... LEO** 09/03/1996 13 STP- Minotau US Technology LEO 23...



Дата загрузки: 2017-03-10
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0.15/5
FACT SHEET Minotaur I Innovation You Can Count OnTM Space Launch Vehicle JAWSAT – Jan 2000 MightySAT II.1 – Jul XSS-11 – Apr 2005 STP-R1 – Sep 2005 COSMIC – Apr 2006 Success on First Five Missions The Minotaur I Space Launch Vehicle The Minotaur I Space Launch Vehicle (SLV) provides a responsive, reliable, and cost-effective launch solution for U.S. Government sponsored spacecraft. In addition to a demonstrated successful history over its initial and subsequent launches, it builds on a long background of dependable launch systems. The Minotaur I uses residual Minuteman II first and second stages in combination with the upper two stages shared with Orbital’s Pegasus XL and Taurus XL commercial SLVs. The Minotaur family of launch vehicles is provided via the Orbital/ Suborbital Program 2 (OSP-2) of the U.S. Air Force Space and Missile 754.7 PAYLOAD FAIRING AVIONICS ASSEMBLY ORION 38 3/4 INTERSTAGE ORION 50XL 2/3 INTERSTAGE Systems Center (SMC) Rocket System Launch Program (RSLP). SR19 Features: • Inertially guided four stage solid rocket propulsion • Flight-proven systems with demonstrated success record • Multiple spaceport launch capability (California, Florida, Alaska, Virginia) using portable ground support equipment FAIRING SEP 580.85 50.0 IN. DIA S2/S3 SEP 340.52 S1/S2 SEP M55 494.75 441.05 52.0 IN. DIA MM 1/2 INTERSTAGE • Full payload integration support including mission management, spacecraft interface support (power, telemetry, sequencing, attitude control, and deployment), and launch operations • Standard 18 month mission response including payload integration and launch by Orbital’s experienced launch crews PAYLOAD I/F 650.15 289.50 274.43 65.76 IN. DIA (Dimensions in Inches) • Responsive launch solutions from 6 months to 48 hours available Minotaur I Space Launch Vehicle 51.79 0.0 Minotaur I Specifications Performance: • Flight-verified system performance • Proven secondary payload capability • Adaptable to a variety of payloads and orbital requirements with typical accuracy of 33.4 nm (3s), 0±0.1 deg inclination (3s) 87.8 22.7 AVAILABLE ENVELOPE (DYNAMIC) • Optional Soft Ride for Small Satellites (SRSS) to mitigate flight dynamics environments • Available optional enhancements include: 151.5 31.0 131.3 47.3 35.4 - Insertion accuracy of <10 nm (3s) inclinations <0.05 deg (3s) AVAILABLE - Conditioned air (Class 10K), temperature and humidity control and nitrogen purge ENVELOPE 0 NOTE: 1. Payload Mass includes Adapter Cone, Separation System and Other Mission-Specific Hardware. 1800 1600 1400 Apogee (km) INTERFACE PLANE 54.7 50.0 2000 INTERFACE PLANE Standard 50” Fairing 0.0 Optional 61” Fairing Payload Accommodations: • Standard 50 in. Pegasus-design payload fairing 1200 • Optional 61 in. fairing for larger or multiple payload missions 1000 • Thermally controlled fairing volume with Class 100K standard cleanliness CCAS 28.5° 800 • Well defined launch environments • Variety of proven payload separation systems available WFF 38° 600 VAFB 72° 400 200 0 (DYNAMIC) 47.0 - Additional payload access panels 80.1 VAFB Sun-Synch 0 100 200 300 400 Kodiak 64° 500 600 Payload (kg) Minotaur I Payload Capability Simplified Horizontal Payload Integration Point of Contact: For Technical Details, Please Contact Us At: Phone: 480.814.6566 E-mail: minotaur@orbital.com Website: www.orbital.com Program Office: Additional information should be obtained from the USAF OSP Office USAF SMC Space Development & Test Wing Rocket System Launch Program (RSLP) 3548 Aberdeen Avenue S.E. Kirtland AFB, NM 87117-5778 (505) 846-8957 FAX: (505) 846-1349 Orbital Sciences Corporation Launch Systems Group 3380 South Price Road Chandler, Arizona 85248 www.orbital.com Innovation You Can Count OnTM © 2006 Orbital Sciences Corporation BR06003



Дата загрузки: 2017-02-23
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0.07/5
FACT SHEET Minotaur I Innovation You Can Count OnTM Space Launch Vehicle JAWSAT – Jan 2000 MightySAT II.1 – Jul 2000 XSS-11 – Apr 2005 STP-R1 – Sep 2005 COSMIC – Apr 2006 TacSat-2 – Dec 2006 Minotaur I Has a Demonstrated Success Record and Flight-Proven Systems The Minotaur I Space Launch Vehicle The Minotaur I Space Launch Vehicle (SLV) provides a responsive, reliable, and cost-effective launch solution for U.S. Government-sponsored spacecraft. It builds on a long background of dependable launch systems and has a demonstrated successful history over its initial and subsequent launches. The Minotaur I SLV uses residual Minuteman II first and second stage rocket motors along with the upper two stages shared with Orbital’s Pegasus XL and Taurus XL commercial SLVs. The combination of decommissioned ICBM motors with commercial boosters and state-of-theart hardware is one of Orbital’s unique strengths from experience spanning several decades. The Minotaur family of launch vehicles are provided via the Orbital/ Suborbital Program 2 (OSP-2) and managed by the U.S. Air Force Space and Missile Systems Center (SMC), Space Development and Test Wing’s (SDTW) 3rd Space Test Squadron (3 STS) located at Kirtland AFB, NM. Features: • Full spacecraft integration support, including mission management, spacecraft interface support (power, telemetry, sequencing, attitude control, and deployment), through launch operations and post-launch performance evaluation. • Standard 18 month mission response including mission integration and launch by Orbital’s uniquely experienced team • Responsive launch solutions from 6 months to a few hours available • Mission success is ensured by mature systems and processes - Orbital’s rigorous mission assurance program - Full Government insight and independent assessment • Multiple spaceport launch capability (California, Florida, Alaska, MidAtlantic) using portable ground support equipment 754.7 SPACECRAFT FAIRING AVIONICS ASSEMBLY ORION 38 3/4 INTERSTAGE ORION 50XL 2/3 INTERSTAGE SR19 PAYLOAD I/F 650.15 FAIRING SEP 580.85 50.0 IN. DIA S2/S3 SEP 441.05 52.0 IN. DIA MM 1/2 INTERSTAGE 340.52 S1/S2 SEP M55 494.75 289.50 274.43 65.76 IN. DIA (Dimensions in Inches) Minotaur I Space Launch Vehicle – Ready to Launch 51.79 0.0 Minotaur I Specifications Performance: • Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km) 2.23 m (87.8 in.) • Typical orbit accuracy of better than ±5 km insertion apse, ±35 km non-insertion apse, and ±0.1 deg inclination (3sigma values) • Optional enhanced insertion accuracy better than 5 km in altitude and ±0.05 deg inclination (3-sigma values) 0.787 m (31.0 in.) AVAILABLE ENVELOPE (DYNAMIC) AVAILABLE ENVELOPE (DYNAMIC) 3.335 m (131.3 in.) 2.035 m (80.1 in.) 1.19 m (47.0 in.) 0 INTERFACE PLANE 1.27 m (50.0 in.) 1.39 m (54.7 in.) INTERFACE PLANE 0.0 1.55 m (61.0 in.) 2000 NOTE: 1. Payload Mass includes Adapter Cone, Separation System and Other Mission-Specific Hardware. 1800 1600 1400 Apogee (km) 3.843 m (151.5 in.) 0.899 m (35.4 in.) 1.20 m (47.3 in.) • Cold gas attitude control system readily accomodates a variety of spacecraft mission requirements, including precise separation pointing and post-boost maneuvers 1200 1000 CCAS 28.5° 800 WFF 38° 600 VAFB 72° 400 200 0 0.576 m (22.7 in.) VAFB Sun-Synch 0 100 200 300 400 Standard 1.27 m (50 in.) Fairing Envelope Optional 1.55 m (61 in.) Fairing Envelope Payload Accommodations: • Standard 1.27 m (50 in.) dia. spacecraft fairing (Pegasus heritage design) • Optional 1.55 m (61 in.) dia. spacecraft fairing for larger and/or multiple spacecraft missions • Mission-specific fairing access doors for spacecraft support • Well-defined launch environments validated with flight data • Various flight-proven spacecraft separation systems available, including low-shock designs • Thermally controlled fairing volume with standard Class M6.5 (100k) cleanliness - Optional Class M5.5 (10k) cleanliness - Optional spacecraft nitrogen purge Kodiak 64° 500 600 Payload (kg) Performance to Orbit Is Flight-Verified and Best in Class Simplified Horizontal Payload Integration for Single and Multiple Spacecraft Program Office: S. A IR F O RC E • U. RSL P MINOTAUR n Orbital Suborbital Program bit al Sc tio Or Additional information should be obtained from the USAF OSP Office USAF SMC Space Development and Test Wing (SDTW) 3rd Space Test Squadron (3 STS) 3548 Aberdeen Avenue S.E. Kirtland AFB, NM 87117-5778 505.846.5911 505.846.6489 • For Technical Details, Please Contact Us At: Phone: 480.814.6566 E-mail: minotaur@orbital.com Website: www.orbital.com NGC Point of Contact: ie n ce s C or p o ra Orbital Sciences Corporation Launch Systems Group 3380 South Price Road Chandler, Arizona 85248 www.orbital.com Innovation You Can Count OnTM © 2006 Orbital Sciences Corporation BR06003b



Дата загрузки: 2016-10-31
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0.06/5
... 2415 PROGRESS M-54 ANIK F1R STP-R1 GPS 2RM-1 CRYOSAT SYRACUSE-3A...-8 BEIDUOU 1D THEMIS IGS 3B STP-1 STPSAT-1 CFESAT FALCONSAT 3 MIDSTAR-1 SKYNET...



Дата загрузки: 2016-11-23
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0.24/5
...: English‬‬ ‫ﳉﻨﺔ ﺍﺳﺘﺨﺪﺍﻡ ﺍﻟﻔﻀﺎﺀ ﺍﳋﺎﺭﺟﻲ‬ ‫ﰲ ﺍﻷﻏﺮﺍﺽ ﺍﻟﺴﻠﻤﻴﺔ‬ ‫ﻣﻌﻠﻮﻣﺎﺕ ﻣﻘ ‪‬ﺪﻣﺔ ﻭﻓﻘﺎ ﻻﺗﻔﺎﻗﻴﺔ ﺗﺴﺠﻴﻞ ﺍﻷﺟﺴﺎﻡ ﺍﳌﻄﻠﻘﺔ‬ ‫ﰲ ﺍﻟﻔﻀﺎﺀ ﺍﳋﺎﺭﺟﻲ‬ ‫ﻣﺬ ﹼﻛﺮﺓ ﺷﻔﻮﻳﺔ ﻣﺆﺭ‪‬ﺧﺔ ‪ ١٧‬ﻛﺎﻧﻮﻥ ﺍﻟﺜﺎﱐ‪/‬ﻳﻨﺎﻳﺮ ‪ ٢٠٠٦‬ﻣﻮ ‪‬ﺟﻬﺔ‬ ‫ﺇﱃ ﺍﻷﻣﲔ ﺍﻟﻌﺎﻡ ﻣﻦ ﺍﻟﺒﻌﺜﺔ ﺍﻟﺪﺍﺋﻤﺔ ﻟﻠﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ ﺍﻷﻣﺮﻳﻜﻴﺔ‬ ‫ﻟﺪﻯ ﺍﻷﻣﻢ ﺍﳌﺘﺤﺪﺓ )ﻓﻴﻴﻨﺎ(‬ ‫‪‬ﺪﻱ ﺍﻟﺒﻌﺜﺔ ﺍﻟﺪﺍﺋﻤﺔ ﻟﻠﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ ﺍﻷﻣﺮﻳﻜﻴﺔ ﻟﺪﻯ ﺍﻷﻣﻢ ﺍﳌﺘﺤﺪﺓ )ﻓﻴﻴﻨﺎ( ﲢﻴ‪‬ﺎ‪‬ﺎ ﺇﱃ‬ ‫ﺍﻷﻣﲔ ﺍﻟﻌﺎﻡ ﻟﻸﻣﻢ ﺍﳌﺘﺤﺪﺓ‪ ،‬ﻭﻳﺸﺮ‪‬ﻓﻬﺎ ﺃﻥ ﲢﻴﻞ ﺇﻟﻴﻪ‪ ،‬ﻭﻓﻘﺎ ﻟﻠﻤﺎﺩﺓ ﺍﻟﺮﺍﺑﻌﺔ ﻣﻦ ﺍﺗﻔﺎﻗﻴﺔ ﺗﺴﺠﻴﻞ‬ ‫ﺍﻷﺟﺴﺎﻡ ﺍﳌﻄﻠﻘﺔ ﰲ ﺍﻟﻔﻀﺎﺀ ﺍﳋﺎﺭﺟﻲ )ﻣﺮﻓﻖ ﻗﺮﺍﺭ ﺍﳉﻤﻌﻴﺔ ﺍﻟﻌﺎﻣﺔ ‪) ٣٢٣٥‬ﺩ‪ ،((٢٩-‬ﺑﻴﺎﻧﺎﺕ‬ ‫ﺗﺴﺠﻴﻞ ﺍﻷﺟﺴﺎﻡ ﺍﻟﻔﻀﺎﺋﻴﺔ ﺍﻟﱵ ﺃﻃﻠﻘﺘﻬﺎ ﺍﻟﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ ﺧﻼﻝ ﺍﻟﻔﺘﺮﺓ ﻣﻦ ﺃﻳﻠﻮﻝ‪/‬ﺳﺒﺘﻤﱪ ﺇﱃ‬ ‫ﺗﺸﺮﻳﻦ ﺍﻟﺜﺎﱐ‪/‬ﻧﻮﻓﻤﱪ ‪) ٢٠٠٥‬ﺍﻧﻈﺮ ﺍﳌﺮﻓﻖ(‪.‬‬ ‫)‪60206 V.06-50444 (A‬‬ ‫*‪*0650444‬‬ ‫‪2‬‬ ‫ﺑﻴﺎﻧﺎﺕ ﺗﺴﺠﻴﻞ ﺍﻷﺟﺴﺎﻡ ﺍﻟﻔﻀﺎﺋﻴﺔ ﺍﻟﱵ ﺃﻃﻠﻘﺘﻬﺎ ﺍﻟﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ ﺍﻷﻣﺮﻳﻜﻴﺔ ﺧﻼﻝ ﺍﻟﻔﺘﺮﺓ ﻣﻦ ﺃﻳﻠﻮﻝ‪/‬ﺳﺒﺘﻤﱪ‬ ‫ﺇﱃ ﺗﺸﺮﻳﻦ ﺍﻟﺜﺎﱐ‪/‬ﻧﻮﻓﻤﱪ ‪*٢٠٠٥‬‬ ‫ﺃﻳﻠﻮﻝ‪/‬ﺳﺒﺘﻤﱪ ‪٢٠٠٥‬‬ ‫ﻳﺴﺘﻜﻤﻞ ﺍﻟﺘﻘﺮﻳﺮ ﺍﻟﺘﺎﱄ ﺑﻴﺎﻧﺎﺕ ﺍﻟﺘﺴﺠﻴﻞ ﺍﳋﺎﺻﺔ ﺑﺎﻷﺟﺴﺎﻡ ﺍﻟﱵ ﺃﻃﻠﻘﺘﻬﺎ ﺍﻟﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ ﺣﱴ ‪ ٣٠‬ﺃﻳﻠﻮﻝ‪/‬ﺳﺒﺘﻤﱪ ‪ .٢٠٠٥‬ﻭﻗﺪ ﹸﺃﺟﺮﻳﺖ ﲨﻴﻊ ﻋﻤﻠﻴﺎﺕ ﺍﻹﻃﻼﻕ‬ ‫ﻣﻦ ﺃﺭﺍﺿﻲ ﺍﻟﻮﻻﻳﺎﺕ ﺍﳌﺘﺤﺪﺓ‪ ،‬ﻣﺎ ﱂ ﻳﺬﻛﺮ ﺧﻼﻑ ﺫﻟﻚ‪.‬‬ ‫ﺍﻟﺘﺴﻤﻴﺔ ﺍﻟﺪﻭﻟﻴﺔ‬ ‫ﺍﺳﻢ ﺍﳉﺴﻢ ﺍﻟﻔﻀﺎﺋﻲ‬ ‫ﺗﺎﺭﻳﺦ ﺍﻹﻃﻼﻕ‬ ‫ﺍﳋﺼﺎﺋﺺ ﺍﻷﺳﺎﺳﻴﺔ ﻟﻠﻤﺪﺍﺭ‬ ‫ﻧﻘﻄﺔ‬ ‫ﺍﻟﻔﺘﺮﺓ ﺍﻟﻌﻘﺪﻳﺔ ﺯﺍﻭﻳﺔ ﺍﳌﻴﻞ‬ ‫ﺍﻷﻭﺝ‬ ‫)ﻛﻢ(‬ ‫)ﺩﺭﺟﺔ(‬ ‫)ﺩﻗﻴﻘﺔ(‬ ‫ﻧﻘﻄﺔ‬ ‫ﺍﳊﻀﻴﺾ‬ ‫)ﻛﻢ(‬ ‫ﺍﻷﺟﺴﺎﻡ ﺍﻟﺘﺎﻟﻴﺔ ﺃﻃﻠﻘﺖ ﺑﻌﺪ ﺻﺪﻭﺭ ﺍﻟﺘﻘﺮﻳﺮ ﺍﻷﺧﲑ ﻭﻻ ﺗﺰﺍﻝ ﻣﻮﺟﻮﺩﺓ ﰲ ﺍﳌﺪﺍﺭ‪:‬‬ ‫‪٩٠,٦‬‬ ‫‪ ٢٣ STP-R1 (USA 185) 2005-037A‬ﺃﻳﻠﻮﻝ‪/‬ﺳﺒﺘﻤﱪ ‪٢٠٠٥‬‬ ‫‪٩٦,٤‬‬ ‫‪٣١٧‬‬ ‫‪٣٠١‬‬ ‫‪2005...



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0.11/5
... и находящиеся на орбите: 2005-037A STP-R1 (USA 185) 23 сентября 2005...



Дата загрузки: 2017-05-21
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0/5
Alphabet Hieroglyph Gardiner G1 Transliteration 1 1 1 or 7 \ M17 M17-M17 or Z4 K G43 q # D58 ! h 1 D36 Q3 I9 G17 t M < $ B N35 b F32 e or B v n ? U ! f S29 or O34 i I10 D21 O4 V28 Aa1 N27 N29 V31 W11 X1 V13 D46 Translation Glottal stop heard in German words (ah) Known As Aleph i ey yodh y a w b p f m n r h H x X s S q k g t T d D yeh y ah ayin ou waw b b p p f f m m n n r r h as in English h hu, emphatic h dotted h ch, like Scotish loch third h ch, like German ich fourth h s s sh shin que, like q in queen backward k k k hard g g t t tu, originally tsh second t d d je, originally dj second d A Dictionary Hieroglyph ! ! ! ! ! !! V 4 !! V !! 8 V !! V 4 !! L !! L V ! FV 1 !! L V !! h 4 !!! !`. !1:` R# ! 1!1 :` !e C 1eC !1 1!E !! 8 !\ K & !\ K ] !\ q ! E Gardiner G1 G1 G1 G1 G1 G1-X1-N5-Z1 G1-X1-N5 G1-X1-Z5-N5 G1-X1-N5-Z1 G1-X1-F9 G1-X1-F9-N5 F3-X1-N5 M17-G1-X1-F9-N5 G1-G1-N23-Z1 G1-G1-X1-G1-D40-A14 G1-M17-Z7-P5 N1-Q3-X1-G17-G1-M17-Z7-P5 G1-S29-Aa2 M17-S29-Aa2 G1-M17-M17-X1-G37 G1-X1-A24 G1-D36-G43-Q6 G1-D36-G43-F27 G1-D36-D58-X1-G37 Transliteration A A A A At At At At At At At At At AA AAtA Aiw pt m Aiw Ais Ais Ayt Ayt Aaw Aaw Aabt Translation enclitic particle vulture, bird in general vulture, bird in general tread striking-power striking-power moment, instant, time in general moment, instant, time moment, instant, time in general moment, instant, time in general moment, instant, time in general moment, instant, time in general moment, instant, time in general mound of ruins Nubian chieftain ? windy ? a windy sky ? viscera viscera blanch ? blanch container for papyri container oppression Other E !\ q ! T 5 jK+ j+ jK jKa jK+5 j!+ j! K+++ j! K+5 j!Kc j!" & ` jK1 18 j:` !j K j:!\ jKK jK 1 18f! 4 jK! \4+5 j:9 jK!> jK<8 ]qn ]qn ]q Kn ]qK' ]q K> G1-D36-D58-X1-F17-G37-Z2 F40-G43-Y1 F40-Y1 F40-G43 F40-G43-D41 F40-G43-Y1-Z2 F40-X1-Y1 F40-X1-G43-Y1-Y1-Y1 F40-X1-G43-Y1-Z2 F40-X1-G43-N18 F40-X1-X2-X6-W22 F40-G43-M17-M17-A24 F40-Z7-D40 G1-F40-G43 F40-Z7-X1-D36 F40-G43-G43 F40-G43-M17-M17-A24-D46-X1-Z1 F40-G43-X1-D36-Z1-Y1-Z2 F40-Z7-Z6 F40-G43-X1-T30 F40-G43-V28-A24 U23-D58-D54 U23-D58-D54 U23-D58-G43-D54 U23-D58-G43-Q7 U23-D58-G43-T30 Aabt Aw Aw Aw Aw Aw Awt Awt Awt Awt Awt Awy Awy Awy Awy Awy Awy Drt Awt a Aw Awt AwH Ab Ab Abw Abw Abw oppression long of space, time adjective long of space, time adjective long, length of space, time length of space noun length of space noun length of time, space length of time gifts, food gifts gifts, food extend, present, announce, arouse extend the arm verb announce someone verb extend the arm verb arouse oneself, masturbate verb lay hands on gifts death long-knife do violence tarry, stray verb intransitive avoid, cease verb transitive cessation brand, scorch brand slaves, cattle ]q!W ]q!-> ]q!`!p5 ]q!` ]q !>!p 5 ]q" :q ]q]q" 8 ]q 118 ]q 11] ]q8 ]K: ]q K: ]qK3 :q K} 3 ]q 3 ]q KU ] q :KP j ]qPj ]q`Q ]KQ ]q :Lj ]Pq `Q ]qB\ U23-D58-X1-Y4-S15 U23-D58-X1-Y3-T30 U23-D58-X1-S24-A1-B1-Z2 U23-D58-X1-S24 U23-D58-X1-T30-A1-B1-Z2 U23-D58-A2 R15-D58 U23-D58-U23-D58-A2 E24 U23-D58-M17-M17-E24 U23-D58-M17-M17-F27 U23-D58-E24 U23-G43-E26 U23-D58-G43-E26 U23-D58-G43-T19 R15-D58-G43-N33A-T19 U23-D58-T19 U23-D58-G43-F18 U23-D58-E26-G43-W6-N25 U23-D58-W6-N25 U23-D58-S24-O49 U23-G43-O49 U23-D58-Z7-Aa2-N25 U23-W6-D58 S24-O49 U23-D58-Aa1-D36 Abt Abt Abt Abt Abt Abi Abi AbAb Aby Aby Aby Aby Abw Abw Abw Abw Abw Abw Abw Abw Abw Abw Abw Abw Abw Abx brand brand noun family family collective noun family collective noun desire, wish for desire, wish for verb be delighted panther panther panther panther elephant elephant ivory ivory ivory ivory Elephantine locality Elephantine locality Elephantine locality Elephantine locality Elephantine locality Elephantine locality Elephantine locality unite, mix, link, mingle, be merged, engage !q B G1-D58-Aa1 ]Bq<+ \ \_ fV4 \_ fN \_ f$ ]q kQ k]Q ]ki :q kKp ]q kKp4 !# < 8 !# fF U23-Aa1-D58-Z9-Y1 G X !# fn !h\ < !h\ < ! !h M 1 1 ' !1 ' !hfo !]18 !1\ F !1\ ! ` !1\ ! \ !1\ K ! ` G39 N11 N11-N14-D46-N5-Z1 N11-N14-D46-W4 N11-N14-D46-X4 U23-D58-N26-O49 N26-U23-O49 U23-N26-N24 R15-D58-N26-G43-K1 U23-D58-N26-G43-K1-Z1 G1-Q3-V28-Z5 G1-Q3-D46-G38 H1 G1-Q3-D46-D54 G1-I9-D36-E28 G1-I9-D36-E28-A1 G1-I9-D21-M17-M17-Q7 G1-G17-Q7 G1-I9-D46-D56 G1-W19-M17-A24 G1-G17-D36-G38 G1-G17-D36-X1-D40 G1-G17-D36-X1-D36 G1-G17-D36-G43-X1-D40 Abx Abx Abd Abd Abd Abd AbDw AbDw AbDw AbDw AbDw ApH Apd Apd Apd link arms verb transitive join a god verb transitive Apd Afa Afa Afry Am Afd Ami Ama Amat Amat Amat rush forward month month monthly festival monthly festival Abydos Abydos locality Abydos locality a fish a fish swine, pigs collective noun duck, bird duck, bird in general duck, bird in general used in offering formula gluttony glutton boil burn, burn up part of animal leg mix a perching bird ramus of jaw, fork of bone, hinged bone ramus of jaw, fork of bone, hinged bone ramus of jaw, fork of bone, hinged bone verb !11i !11! i !11K \ 5 !aeE5 !aet !M,8 1 M,` !1 M,8 !M1 1!s !M!R !$ 1 1 n !$ K E !$ E 1$:E5 1 ...