Ракетный блок. H10. [Редактировать]

Технические характеристики

#ХарактеристикаЗначение
1Длина, метра9.9
2Стартовая масса, кг12036
3Тяга, кН62,7
4Удельный импульс, с444.2
5Время работы, с780
6Масса (сухая), кг1336
7Двигательные установки 1xHM-7B
8Горючееводород
9Окислителькислород
10Диаметр, метра2.8

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Distributing And- and Or-Work in the Andorra-I Parallel Logic Programming System In ˆes de Castro Dutra A thesis submitted to the University of Bristol in accordance w ith the requirements for the degree of Doctor of Philosophy in the Faculty of Engineering, Department of Computer Science. February 1995 Abstract Parallelism and logic programming are tw o fi elds that have been successfully combined, as is show n by recent implementations of parallel logic programming systems. There are tw o main sources of parallelism in logic programming, namely or-parallelism and and-parallelism. Or-parallelism is exploited w hen several alternative clauses to a goal are executed in parallel. And-parallelism is exploited w hen w e execute tw o or more goals of the same clause simultaneously. Exploitation of full or-parallelism and and-parallelism is limited by the number of physical processors available in a system. And-parallelism is also limited by the interdependence among goals in a clause. In parallel logic programming systems w hich exploitboth and-parallelism and or-parallelism, a problem that arises is how to distribute processors betw een the dynamically varying amounts of and-w ork and or-w ork that are available. Solutions have been reported for distributing only or-w ork, or distributing only and-w ork, but the issue of distributing processors betw een both kinds of w ork has not yet been addressed. In this thesis w e discuss the problem of distributing and-w ork and or-w ork in the context of Andorra-I, a parallel logic programming system that exploits determinate and-parallelism and or-parallelism, and propose scheduling strategies that aim at effi ciently distributing processors betw een and-w ork and or-w ork. We study general criteria that every scheduling strategy should meet to reconfi gure processors w ithout incurring too high overheads in the Andorra-I system. We propose tw o different strategies to reconfi gure processors betw een and-w ork and or-w ork based on these criteria. One strategy, work-guided, guides its decisions by looking at the amount of current and-w ork and or-w ork available in an application during execution. The other strategy, effi ciency-guided, is designed around the intuition that processors should spend most of their execution time doing useful w ork, i.e., performing reductions. Our benchmark setconsists of programs thatcontain both and-parallelism and or-parallelism and programs that contain a single kind of parallelism. We compare the results produced by our strategies w ith the results produced by a version of Andorra-I that provides only a fi xed division of processors betw een and-w ork and or-w ork. Results show the benefi t of adding a reconfi gurer to Andorra-I and show that both strategies perform better than any plausible fi xed confi guration for all benchmarks. Although our w ork is focussed on the Andorra-I system, w e believe that both strategies could be applied to other parallel logic programming systems that aim at exploiting both and-parallelism and or-parallelism. Declaration No portion of the w ork referred to in this thesis has been submitted in support of an application for another degree or qualifi cation of this or any other university or institution of learning. Inˆe s de Castro Dutra Acknowledgements Several people have contributed to the realisation of this w ork and for my (in) formation in the logic programming fi eld. I w ould like to express my gratitude to my advisor, David H. D. Warren, for providing me w ith guidance, support and understanding. His insightful comments and suggestions regarding the presentation and content of this dissertation have improved it greatly. Logic Programming w as fi rst introduced to me by my ex-supervisor, Claudio Amorim, w hile I w as doing my M.Sc. course in UFRJ/ Brasil. After that I got to know the mysteries of the PLM and WAM abstract machines through Priscila that had all the patience in teaching me everything she arduously got to know facing several diffi culties and very hard w ork. Ricardo, alw ays in a very good humoured mood, w as of very much help and support during the time w e w orked together in the Prolog project. I am indebted to the members of the Gigalips project, particularly David Warren, V´ı tor Santos Costa, Rong Yang, Tony Beaumont, Ra´e d Sindaha, Gopal Gupta and Kish Shen, for their invaluable comments and discussions. David, my advisor, w as of great support during all my stay in Bristol. He w as alw ays ready to discuss about any question and encouraged me to carry on this w ork. V´ı tor has been my “ guru” in all aspects of computer science. His know ledge of Unix systems and computer science in general made me think that I had to go back to the university and learn everything again properly! I learned very much from him. Rong, w ith her kindness “ saved” me several times w hile I w as running programs in Andorra-I. Tony w as also alw ays friendly and helped me to understand the or-...



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ISSI Scientific Report SR-007 Calibration of Particle Instruments in Space Physics M. Wüest, D. S. Evans & R. von Steiger (Eds.) SR-007 September 2007 Calibration of Particle Instruments in Space Physics Editors Martin W¨uest INFICON Ltd, Balzers, Principality of Liechtenstein David S. Evans Space Environment Center, NOAA, Boulder CO, USA Rudolf von Steiger International Space Science Institute, Bern, Switzerland ii Cover: Example calibration data of the ASPERA-4/ELS sensor on the Venus Express mission of ESA (see p. 145). The International Space Science Institute is a Foundation under Swiss law. It is funded by the European Space Agency, the Swiss Confederation, the Swiss National Science Foundation, and the University of Bern. For more information about ISSI see www.issibern. ch. Published for: by: Publication Manager: Cover Design: Copyright: ISSN: Price: The International Space Science Institute Hallerstrasse 6, CH-3012 Bern, Switzerland ESA Publications Division Keplerlaan 1, 2200 AG Noordwijk, The Netherlands Karen Fletcher N.N. c 2007 ISSI/ESA ZZZZ-YYYX XX Euros Contents List of Figures xi List of Tables xvii Preface xix 1 2 Introduction 1.1 Particle Environments . . . . . . . . . 1.2 Measurement Requirements . . . . . 1.3 Conversion to Physical Quantities . . 1.3.1 Particle Fluxes . . . . . . . . 1.3.2 Velocity Distribution Function 1.3.3 Moments . . . . . . . . . . . 1.3.4 Gas Densities . . . . . . . . . 1.4 Required Accuracy . . . . . . . . . . 1.5 Error Sources . . . . . . . . . . . . . Bibliography . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1 1 5 5 5 6 7 7 8 10 Review of Instruments 2.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.1 Important Characteristics of Analyzers . . . . . . 2.2 Detectors . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Faraday Cups . . . . . . . . . . . . . . . . . . . . 2.2.2 Discrete Electron Multiplier . . . . . . . . . . . . 2.2.3 Continuous Electron Multiplier . . . . . . . . . . 2.2.4 Microchannel Plates . . . . . . . . . . . . . . . . 2.2.5 Solid-State Detectors . . . . . . . . . . . . . . . . 2.2.5.1 Energy Loss of Particles in Matter . . . 2.2.5.2 Silicon Solid-State Detectors . . . . . . 2.2.5.3 Scintillators and Cherenkov Radiators . 2.2.6 Avalanche Photo Diodes . . . . . . . . . . . . . . 2.3 Langmuir Probes . . . . . . . . . . . . . . . . . . . . . . 2.3.1 Overview of the Langmuir Probe Technique . . . . 2.3.2 Types of Probes Used in Ionosphere Measurements 2.3.3 Measurement Accuracy . . . . . . . . . . . . . . 2.3.4 Internal Consistency Checks . . . . . . . . . . . . 2.3.5 Implementation Issues . . . . . . . . . . . . . . . 2.3.5.1 Boom Mounting . . . . . . . . . . . . . 2.3.5.2 Collector Surfaces . . . . . . . . . . . . 2.3.5.3 Probe Contamination . . . . . . . . . . 2.3.5.4 Magnetically Induced Potentials . . . . 2.3.5.5 Adaptive Circuitry . . . . . . . . . . . . 2.3.5.6 Spacecraft Design Factors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 11 13 13 13 14 15 18 27 27 29 32 34 34 35 36 37 37 38 38 38 39 39 39 40 iii . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv C ONTENTS 2.4 2.5 2.6 2.7 2.8 2.9 2.3.6 Summary of Langmuir Probe Operations in Dense Plasmas . 2.3.7 Langmuir Probe Measurements in Low Density Plasmas . . Faraday Cups . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4.2 Instrument Description . . . . . . . . . . . . . . . . . . . . 2.4.2.1 System Components . . . . . . . . . . . . . . . . 2.4.2.2 Measurement Chain . . . . . . . . . . . . . . . . Plasma Analyzers . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5.2 The Retarding Potential Analyzer . . . . . . . . . . . . . . 2.5.3 The Cylindrical Curved Plate Electrostatic Analyzer . . . . 2.5.4 Spherical Sector Analyzers . . . . . . . . . . . . . . . . . . 2.5.5 Top-Hat Analyzers . . . . . . . . . . . . . . . . . . . . . . 2.5.5.1 Spherical Top-Hat Analyzers . . . . . . . . . . . 2.5.5.2 Toroidal Top-Hat Analyzers . . . . . . . . . . . . 2.5.5.3 Electrostatic Deflection to Increase Field of View 2.5.6 Magnetic Sector Analyzers . . . . . . . . . . . . . . . . . . 2.5.7 Plasma Analyzer Summary . . . . . . . . . . . . . . . . . . Mass ...



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SR-007 September 2007 Calibration of Particle Instruments in Space Physics Editors Martin W¨uest INFICON Ltd, Balzers, Principality of Liechtenstein David S. Evans Space Environment Center, NOAA, Boulder CO, USA Rudolf von Steiger International Space Science Institute, Bern, Switzerland ii Cover: Example calibration data of the ASPERA-4/ELS sensor on the Venus Express mission of ESA (see p. 149). The International Space Science Institute is a Foundation under Swiss law. It is funded by the European Space Agency, the Swiss Confederation, the Swiss National Science Foundation, and the University of Bern. For more information about ISSI see www.issibern. ch. Published for: by: Publication Manager: Cover Design: Copyright: ISSN: Price: The International Space Science Institute Hallerstrasse 6, CH-3012 Bern, Switzerland ESA Publications Division Keplerlaan 1, 2200 AG Noordwijk, The Netherlands Karen Fletcher N.N. c 2007 ISSI/ESA ZZZZ-YYYX XX Euros Contents Preface 1 2 xix Introduction 1.1 Particle Environments . . . . . . . . . 1.2 Measurement Requirements . . . . . 1.3 Conversion to Physical Quantities . . 1.3.1 Particle Fluxes . . . . . . . . 1.3.2 Velocity Distribution Function 1.3.3 Moments . . . . . . . . . . . 1.3.4 Gas Densities . . . . . . . . . 1.4 Required Accuracy . . . . . . . . . . 1.5 Error Sources . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1 1 5 5 5 6 7 7 8 Review of Instruments 2.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.1 Important Characteristics of Analyzers . . . . . . . . . . 2.2 Detectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Faraday Cups . . . . . . . . . . . . . . . . . . . . . . . . 2.2.2 Discrete Electron Multiplier . . . . . . . . . . . . . . . . 2.2.3 Continuous Electron Multiplier . . . . . . . . . . . . . . 2.2.4 Microchannel Plates . . . . . . . . . . . . . . . . . . . . 2.2.5 Solid-State Detectors . . . . . . . . . . . . . . . . . . . . 2.2.5.1 Energy Loss of Particles in Matter . . . . . . . 2.2.5.2 Silicon Solid-State Detectors . . . . . . . . . . 2.2.5.3 Scintillators and Cherenkov Radiators . . . . . 2.2.6 Avalanche Photo Diodes . . . . . . . . . . . . . . . . . . 2.3 Langmuir Probes . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3.1 Overview of the Langmuir Probe Technique . . . . . . . . 2.3.2 Types of Probes Used in Ionosphere Measurements . . . . 2.3.3 Measurement Accuracy . . . . . . . . . . . . . . . . . . 2.3.4 Internal Consistency Checks . . . . . . . . . . . . . . . . 2.3.5 Implementation Issues . . . . . . . . . . . . . . . . . . . 2.3.5.1 Boom Mounting . . . . . . . . . . . . . . . . . 2.3.5.2 Collector Surfaces . . . . . . . . . . . . . . . . 2.3.5.3 Probe Contamination . . . . . . . . . . . . . . 2.3.5.4 Magnetically Induced Potentials . . . . . . . . 2.3.5.5 Adaptive Circuitry . . . . . . . . . . . . . . . . 2.3.5.6 Spacecraft Design Factors . . . . . . . . . . . . 2.3.6 Summary of Langmuir Probe Operations in Dense Plasmas 2.3.7 Langmuir Probe Measurements in Low Density Plasmas . 2.4 Faraday Cups . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 11 13 13 13 14 15 18 27 27 29 32 34 34 35 36 37 37 38 38 38 39 39 39 40 41 41 43 43 iii . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv C ONTENTS 2.4.2 Instrument Description . . . . . . . . . . . . . . . . . . . . 2.4.2.1 System Components . . . . . . . . . . . . . . . . 2.4.2.2 Measurement Chain . . . . . . . . . . . . . . . . 2.5 Plasma Analyzers . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5.2 The Retarding Potential Analyzer . . . . . . . . . . . . . . 2.5.3 The Cylindrical Curved Plate Electrostatic Analyzer . . . . 2.5.4 Spherical Sector Analyzers . . . . . . . . . . . . . . . . . . 2.5.5 Top-Hat Analyzers . . . . . . . . . . . . . . . . . . . . . . 2.5.5.1 Spherical Top-Hat Analyzers . . . . . . . . . . . 2.5.5.2 Toroidal Top-Hat Analyzers . . . . . . . . . . . . 2.5.5.3 Electrostatic Deflection to Increase Field of View 2.5.6 Magnetic Sector Analyzers . . . . . . . . . . . . . . . . . . 2.5.7 Plasma Analyzer Summary . . . . . . . . . . . . . . . . . . 2.6 Mass Spectrometers . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6.1 Performance Specifications . . . . . . . . . . . . . . . . . . 2.6.2 Introduction to Magnetic and Electric Analyzers . . . . . . 2.6.2.1 Magnetic Mass ...



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... I: V10 I: V18 I: V23 I: V36 I: H6 I: H10 I: H18 I: H23 I: H36 Γ: H6, V6... : H6, H10, V6, V10 I: H6, H10, V6, V10 ; Tb : H6, H10, V6, V10, H23, H36, V36 I: H6, H10..., V6, V18, V23, V36, H10 I & Tb : H6, H10, H18, H23, H36, H89..., V23, V36, V89 Tb : H6, H10, H18, H23, H36, H89, V6..., V18, V23, V36, V89 I: H6, H10, H18, H23, H36, H89, V6...



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... Island (Cape Verde). 5* H10 Provença Hotel, Barcelona. 4* H10 Villa de la Reina..., Lisbon (Portugal). Refurbishment of the 4* H10 Tribeca Hotel at C/ Pedro Teixeira.... Álvaro Sanz and HCP. 38 5* H10 PROVENÇA HOTEL, BARCELONA (SPAIN) Built... by Jaime Beriestain. 39 BUILDING 4* H10 VILLA DE LA REINA, MADRID... Parque das Nações, Lisbon. 4* H10 Lisbon Hotel at Avenue Duque... of Olivais, Lisbon Refurbishment of 4* H10 Hotel, Lisbon EB1 (1st cycle...



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... Standards Models: H10-13.4, H10-30, H10-20, H20-10, H10-60, H10-56, 10S... comfort feature Models: H10-13 XL/XP, H10-56 HXL/HXP, H20.../DO-214 Standards Models: H10-76XL, H10-66, H10-66XL HEARING PROTECTORS: Models...



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...żenie 8 9 10 11 12 HEPA H10 Teleskopowa z metalową podstawą + + + – HEPA H13... VC3100.0HP) B Filtr wlotowy HEPA H10 (zamontowany w odkurzaczu VC3100.0SK) 15... HEPA (High Efficiency Particulate Air) H10 lub H13. Są to filtry o wyj... wszystkie cząsteczki kurzu. Klasy H10 i H13 określają przepuszczalność danego filtra: filtr H10 zatrzymuje 85% cząsteczek o wielko...áč Parketový kartáč „BNB“ 1600 W + + + HEPA H10 Teleskopická s kovovým podstavcem + + + – VC3100.0HP...či VC3100.0HP) B Vstupní filtr HEPA H10 (namontovaný ve vysavači VC3100.0SK... HEPA (High Efficiency Particulate Air) H10 nebo H13. Jsou to filtry...žet téměř všechny částice prachu. Třídy H10 a H13 označují propustnost daného filtru: filtr H10 zadržuje 85% částic o velikosti... 1 VC3100.0SK 1600 W + + + Teleskopická HEPA H10 s kovovým podstavcom rúrka VC3100.0HP...ým podstavcom rúrka + + + + B Vstupný filter HEPA H10 (namontovaný do vysávača VC3100... HEPA (High Efficiency Particulate Air) H10 alebo H13. To sú filtre o výnimo... mikročastice nečistôt . Triedy H10 a H13 určujú priepustnosť daného filtra: filter H10 zdržuje 85% častíc väčších... 12 VC3100.0SK 1600 W + + + HEPA H10 Teleszkópos fém alappal + + + – VC3100.0HP... típusú porszívóba szerelve) B HEPA H10 bemeneti szűrő (a VC3100.0SK típus...ívók HEPA (High Efficiency Particulate Air) H10 vagy H13 osztályú kimeneti... szinten minden porszemet kiszűrni. A H10 és H13 osztály a szűrő szűrőképességét jelzik: a H10 szűrő a 0,3 mikron nagyságú szennyeződések... 12 VC3100.0SK 1600 W + + + HEPA H10 Telescopică cu suport de metal... VC3100.0HP) B Filtru intrare HEPA H10 (montat în aspiratorul VC3100.0SK) 15... HEPA (High Efficiency Particulate Air) H10 sau H13. Aceste filtre au... toate particolele de praf. Clasele H10 şi H13 definesc permeabilitatea filtrului respectiv: filtrul H10 reţine 85% de particole... основанием + + + + VC3100.0SK 1600 W + + + HEPA H10 Телескопическая VC3100.0HP 1600 W + + + HEPA... VC3100.0HP) B Впускной фильтр HEPA H10 (установлен в пылесосе VC3100.0SK) 15... (High Efficiency Particulate Air) H10 или H13. Это фильтры с исключительно... почти все частички пыли. Классы H10 и H13 обозначают пропускную способность данного фильтра: фильтр H10 задерживает 85% частичек величиной 0,3 микрона... и оборудване 8 9 10 11 12 HEPA H10 Телескопична с метална подставка + + + – HEPA H13... оснащення 8 9 10 11 12 HEPA H10 Телескопічна з металевою основою + + + – HEPA...і VC3100.0HP) B Впускний фільтр HEPA H10 (встановлений у пилососі VC3100.0SK) 15... (High Efficiency Particulate Air) H10 або H13. Це фільтри з винятково... майже всі частинки пилу. Класи H10 і H13 означають пропускну здатність даного фільтра: фільтр H10 затримує 85% частинок розміром... rūšis 7 8 9 10 11 12 HEPA H10 Teleskopinis su metaliniu pagrindu + + + – HEPA....0HP siurblyje) B Pagrindiniu filtru HEPA H10 (montuojamu VC3100.0SK siurblyje) 50... klasės (High Efficiency Particulate Air) H10 arba H13 oro įtraukimo filtrais... sulaikyti bemaž visas dulkių dalelytes. H10 ir H13 klasės apibrėžia filtrų pralaidumo laipsnį: H10 filtras sulaiko 85% dalelyčių, kuri...īkojums 7 8 9 10 11 12 HEPA H10 Teleskopiskā Ar metāla pamatu....0HP) B Ieplūdes filtrs HEPA H10 (iemontēts putekļusūcējā VC3100... filtru (High Efficiency Partuclate Air) H10 un H13. Filtri atšķiras...ēt gandrīz visas putekļu daļiņas. H10 un H13 klasifikatori raksturo filtra apturēšanas spēju: filtrs H10 aptur 85% daļiņu, kuru lielums... varustus 7 8 9 10 11 12 HEPA H10 Teleskoop metallist + + + – HEPA H13 Teleskoop... VC3100.0HP sissemonteeritud) B Mootorifilter HEPA H10 (tolmuimeja mudelis VC3100.0SK sissemonteeritud... (High Efficiency Particulate Air) õhufiltriga H10 või H13. Need on erakordselt suure... peaaegu kõik tolmuosakesed. Filtrite klassid H10 ja H13 näitavad filtrite läbilaskevõimet: filter H10 peab kinni 85% osakestest suurusega... 12 VC3100.0SK 1600 W + + + HEPA H10 Telescopic with metal base + + + – VC3100... VC3100.0HP) B Inlet filter HEPA H10 (mounted in vacuum cleaner VC3100... (High Efficiency Particulate Air) type H10 or H13. These filters have... dust particles. The filter standards H10 and H13 define the permeability of the filter: H10 filter can retain 85% of...



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... DAVID CLARK HEADSETS DAVID CLARK H10-13.4 HEADSET Provides David Clark... warranty. P/N H10-13.4...............................................................................$320.85 P/N H10-13.4S (stereo) .............................................................. $325.50 P/N H10-13H... cord)................................. $338.52 DAVID CLARK H10-13Y YOUTH HEADSET Same features as the popular H10-13.4 Headset and has been... convert your H10-13Y to a David Clark Model H10-13.4 ..........P/N H10-13Y ........$320...-13091........................$310.00 DAVID CLARK H10-56HXL HELICOPTER HEADSETS New Comfort... used with optional panel mount. (H10-56HXP) Dual volume controls let...): 22 oz. Description MODEL H10-56HXL MODEL H10-56HXP Part No. Price... 11-03829 $737.49 MODEL H10-56 - Hinged wire boom with... Change Without Notice DAVID CLARK H10-76 LOW IMPEDANCE HEADSET Undercut... the United States, use the H10-76 both in the cockpit....00 DAVID CLARK H10-13X ANR HEADSETS The H10-13X aviation headset... popular and comfortable headset style. H10-13X Features: Quiet Performance —You... headset (ENC) with straight, 5ft. H10- cord to Battery Power Module..., Snap Lock-Quick Release Connector/ H10- Battery Power Module with mating... Headset (ENC) with straight, 5ft. H10- cord, Snap lock-Quick Release...) cord, Snap Lock-Quick Release H10- Connector/Battery Power Module with... $725.40 PS DAVID CLARK H10-13X CIGARETTE POWER CABLE The David Clark H10-13XP Cigarette Power for the H10-13XP Headset. P/N 11-04790.............$42.... CLARK HEADSETS DAVID CLARK HEADSET H10-66LX & H10-76XL CM WP ME... Aviation. Description Part No. Price H10-66XL DUAL IMPEDANCE ENC HEADSET... technology and enhanced comfort features. H10-76XL PORTABLE LOW IMPEDANCE ENC... noise attenuation with ENC activated. H10-76XP PANEL-MOUNT LOW IMPEDANCE ENC HEADSET Same as H10-76XL but with permanent panel... 11-05429 $773.76 source. H10-20 HEADSET 8 new headset design advances make the David Clark H10-20 a must see. The completely... .............P/N H10-20.............$316.20 Coiled Cord ...............P/N H10-21.............$344.10 Helicopter ..................P/N H10-26....94 EP CS DAVID CLARK H10-30 HEADSET IN This dual... EL AV DAVID CLARK H10-36 HEADSET The H10-36 headset features... helicopter installations. P/N H10-36 ............$283.65 DAVID CLARK H10-60 HEADSET Features... amplified electret mic. Customize your H10-60 with 3-position headset pressure... size adjustment, and cord selection. P/N H10-60 ........................ $366.42 TO PS DAVID CLARK H10-66 HEADSET A unique dual impedance... military style aircraft. The Model H10-66 features include new comfort... Rating (NRR) of 27 dB. P/N H10-66 ...................... $398.97 BV DAVID CLARK H10-76 HEADSET Undercut Comfort-Gel... .................. $290.16 718 DAVID CLARK H10-00 “LISTEN ONLY” HEADPHONE David... to 6 ft, & PJ-055B plug. P/N H10-00 ........................ $217.62 DAVID CLARK...-Head style (Except H20-10 & H10-80) headsets into a Helmet/ Headset... the following headsets (H10-13.4, H10-20, H10-30, H10-56, and H10-60) ** All... David Clark Headsets. David Clark H10 Comfort Gel Undercut Ear 11... - Increases the versatility of the H10-60 headset. Plugs into the... - Increases the versatility of the H10-60 headset. Plugs into the... Increases the versatility of the H10-60 headset. Plugs into the...-06310..............$169.95 David Clark H10-76 P/N 11-07808.............$169.95...