natgillin/translations-raw huggingface dataset:
The glass transition temperature (Tg) for 1C008 materials is determined using the method described in ASTM D 3418 using the dry method.
Točka posteklenitve (Tg) pri materialih iz točke 1C008 se določa z uporabo suhe metode, opisane v ASTM D 3418.
Unprocessed fluorinated compounds, as follows:
Nepredelane fluorirane spojine:
Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching;
kopolimeri viniliden fluorida, ki vsebujejo 75 % ali več beta kristalinske strukture v neraztegnjenem stanju;
Fluorinated polyimides containing 10 % by weight or more of combined fluorine;
fluorirani poliamidi, ki vsebujejo 10 ut. % ali več kombiniranega fluora;
Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine.
fluorirani elastomeri fosfazena, ki vsebujejo 30 ut. % ali več kombiniranega fluora.
"Fibrous or filamentary materials" which may be used in organic "matrix", metallic "matrix" or carbon "matrix""composite" structures or laminates, as follows:
"Vlakneni ali nitasti materiali", ki se lahko uporabijo v "kompozitnih" strukturah organske "matrike", kovinske "matrike" ali ogljikove "matrike" ali v laminatih:
N.B.: SEE ALSO 1C210.
NAPOTILO: GLEJ TUDI TOČKO 1C210.
Organic "fibrous or filamentary materials", having all of the following:
organski "vlakneni ali nitasti materiali", ki imajo vse naslednje značilnosti:
A "specific modulus" exceeding 12,7 × 106 m; and
"specifičnim modulom", večjim od 12,7 × 106 m; in
A "specific tensile strength" exceeding 23,5 × 104 m;
"specifično natezno trdnost", večjo od 23,5 × 104 m;
Note: 1C010.a. does not control polyethylene.
Opomba: Predmet nadzora iz točke 1C010.a. ni polietilen.
Carbon "fibrous or filamentary materials", having all of the following:
ogljikovi "vlakneni ali nitasti materiali", ki imajo vse naslednje značilnosti:
Note: 1C010.b. does not control fabric made from "fibrous or filamentary materials" for the repair of aircraft structures or laminates, in which the size of individual sheets does not exceed 50 cm × 90 cm.
Opomba: Predmet nadzora iz točke 1C010.b niso izdelki, izdelani iz "vlaknenih ali nitastih materialov", ki se uporabljajo pri popravilu delov zračnih plovil ali laminatov, če velikost posamezne plošče ne presega 50 cm × 90 cm.
Properties for materials described in 1C010.b. should be determined using SACMA recommended methods SRM 12 to 17, or national equivalent tow tests, such as Japanese Industrial Standard JIS-R-7601, Paragraph 6.6.2., and based on lot average.
Značilnosti materialov, opisanih v točki 1C010.b, se določajo z uporabo metod z oznakami SRM 12 do 17, ki jih priporoča "Suppliers Advance Composite Materials Association" (SACMA), ali z uporabo enakovrednih nacionalnih nateznih preskusov, kakor so "Japanese Industrial Standard" JIS-R-7601, odstavek 6.6.2, ki temeljijo na povprečju velikega števila vzorcev.
Inorganic "fibrous or filamentary materials", having all of the following:
anorganski "vlakneni ali nitasti materiali", ki imajo vse naslednje značilnosti:
A "specific modulus" exceeding 2,54 × 106 m; and
"specifičnim modulom", večjim od 2,54 × 106 m; in
A melting, softening, decomposition or sublimation point exceeding 1922 K (1649 °C) in an inert environment;
tališče, točko razgraditve ali sublimišče nad 1922 K (1649 °C) v inertnem okolju;
Note: 1C010.c. does not control:
Opomba: Predmet nadzora točke 1C010.c niso:
Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 weight percent or more silica, with a specific modulus of less than 10 × 106m;
nekontinuirana, mnogofazna, polikristalinska aluminijeva vlakna, narezana ali v naključnem prepletu, ki vsebujejo 3 ut. % ali več silicija, in katerih "specifični modul" je manj kakor 10 × 106 m;
Molybdenum and molybdenum alloy fibres;
molibdenska vlakna ali vlakna njegovih zlitin;
Boron fibres;
borova vlakna;
Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2043 K (1770 °C) in an inert environment.
nekontinuirana keramična vlakna s tališčem, točko razgraditve ali sublimiščem pod 2043 K (1770 °C) v inertnem okolju.
"Fibrous or filamentary materials":
"vlakneni ali nitasti materiali":
Composed of any of the following:
ki so sestavljeni iz katerega koli od naslednjih materialov:
Polyetherimides specified in 1C008.a.; or
iz polieterimidov, naštetih v točki 1C008.a; ali
Materials specified in 1C008.b. to 1C008.f.; or;
iz materialov, naštetih v točkah 1C008.b do 1C008.f; ali;
Composed of materials specified in 1C010.d.1.a. or 1C010.d.1.b. and "commingled" with other fibres specified in 1C010.a., 1C010.b. or 1C010.c.;
ki so sestavljeni iz materialov, naštetih v točki 1C010.d.1.a ali 1C010.d.1.b, in "vmešani" z drugimi vlakni, naštetimi v točkah 1C010.a, 1C010.b ali 1C010.c;
Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or "carbon fibre preforms", as follows:
vlakna, ki so impregnirana z umetnimi ali naravnimi smolami (prepregi), vlakna, prevlečena s kovino ali ogljikom (predoblike), ali "predoblike ogljikovih vlaken":
Made from "fibrous or filamentary materials" specified in 1C010.a., 1C010.b. or 1C010.c.;
iz "vlaknenih ali nitastih materialov", ki so določeni v točkah 1C010.a, 1C010.b ali 1C010.c;
Made from organic or carbon "fibrous or filamentary materials":
iz organskih ali ogljikovih "vlaknenih ali nitastih materialov":
With a "specific tensile strength" exceeding 17,7 × 104 m;
s "specifično natezno trdnostjo", večjo od 17,7 × 104 m;
With a "specific modulus" exceeding 10,15 × 106 m;
s "specifičnim modulom", večjim od 10,15 × 106 m;
Not controlled by 1C010.a. or 1C010.b.; and
ki niso določeni v točkah 1C010.a ali 1C010.b; in
When impregnated with materials specified in 1C008 or 1C009.b., having a glass transition temperature (Tg) exceeding 383 K (110 °C) or with phenolic or epoxy resins, having a glass transition temperature (Tg) equal to or exceeding 418 K (145 °C).
imajo, kadar so impregnirani z materiali, določenimi v 1C008 ali 1C009.b, točko posteklenitve (Tg) višjo od 383 K (110 °C), kadar pa so impregnirani s fenolnimi ali epoksi smolami, imajo točko posteklenitve (Tg) enako ali višjo od 418 K (145 °C).
Notes: 1C010.e. does not control:
Opombe: Predmet nadzora točke 1C010.e niso:
Epoxy resin "matrix" impregnated carbon "fibrous or filamentary materials" (prepregs) for the repair of aircraft structures or laminates, in which the size of individual sheets of prepreg does not exceed 50 cm × 90 cm;
"vlakneni ali nitasti materiali", impregnirani z "matriko" epoksi smol (prepregi) ki se uporabljajo pri popravilu delov zračnih plovil ali laminatov, če velikost posamezne plošče ne presega 50 cm × 90 cm;
Prepregs when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature.
prepregi, če so impregnirani s fenolnimi ali epoksi smolami, ki imajo točko posteklenitve (Tg) pod 433 K (160 °C) in temperaturo procesa pod točko posteklenitve.
The glass transition temperature (Tg) for 1C010.e. materials is determined using the method described in ASTM D 3418 using the dry method.
Temperaturna točka posteklenitve (Tg) pri materialih iz točke 1C010.e se določa z uporabo suhe metode, opisane v ASTM D 3418.
The glass transition temperature for phenolic and epoxy resins is determined using the method described in ASTM D 4065 at a frequency of 1 Hz and a heating rate of 2 K (°C) per minute using the dry method.
Temperaturna točka posteklenitve je za fenolne in epoksi smole določena z uporabo suhega postopka, ki je opisan v ASTM D 4065, pri frekvenci 1 Hz in hitrosti segrevanja 2 K (°C) na minuto.
Metals and compounds, as follows:
Kovine in spojine:
N.B.: SEE ALSO MILITARY GOODS CONTROLS and 1C111.
NAPOTILO: GLEJ TUDI NADZOR VOJAŠKEGA BLAGA in TOČKO 1C111.
Metals in particle sizes of less than 60 μm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys of these;
kovine z velikostjo delcev manj kakor 60 μm, bodisi sferične, atomizirane, sferoidne, v kosmičih ali drobljene, izdelane iz materiala, ki vsebuje 99 % ali več cirkonija, magnezija ali njunih zlitin;
The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.
Naravna vsebnost hafnija v cirkoniju (značilna je od 2 % do 7 %) se šteje skupaj s cirkonijem.
Note: The metals or alloys listed in 1C011.a. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.
Opomba: Kovine ali zlitine iz točke 1C011.a so predmet nadzora ne glede na to, ali so kovine ali zlitine vdelane v aluminij, magnezij, cirkonij ali berilij ali ne.
Boron or boron carbide of 85 % purity or higher and a particle size of 60 μm or less;
bor ali borov karbid s čistoto 85 % ali več in z delci velikosti 60 μm ali manj;
Note: The metals or alloys listed in 1C011.b. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.
Opomba: Kovine ali zlitine iz točke 1C011.b so predmet nadzora ne glede na to, ali so kovine ali zlitine vdelane v aluminij, magnezij, cirkonij ali berilij ali ne.
Guanidine nitrate;
gvanidin nitrat;
Materials as follows:
Materiali:
These materials are typically used for nuclear heat sources.
Ti materiali se navadno uporabljajo kot jedrski toplotni viri.
Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50 % by weight;
plutonij v kateri koli obliki, v katerem je več kakor 50 ut. % deleža plutonija z izotopskim številom 238;
Note: 1C012.a. does not control:
Opomba: Predmet nadzora točke 1C012.a niso:
Shipments with a plutonium content of 1 g or less;
dobave, ki vsebujejo 1 g ali manj plutonija;
Shipments of 3 "effective grammes" or less when contained in a sensing component in instruments.
dobave s tremi "efektivnimi grami" ali manj plutonija, kadar jih vsebujejo senzorji merilnih instrumentov.
"Previously separated" neptunium-237 in any form.
"predhodno ločeni" neptunij 237 v kateri koli obliki.
Note: 1C012.b. does not control shipments with a neptunium-237 content of 1 g or less.
Opomba: Predmet nadzora točke 1C012.b niso dobave, ki vsebujejo 1 g ali manj neptunija 237.
Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in "missiles" and their subsystems.
Materiali in naprave za zmanjšano opaznost, kakor je radarska odbojnost, ultravijolični/infrardeči znaki in zvočni znaki, razen tistih iz točke 1C001, ki se uporabljajo v "projektilih" in njihovih podsistemih.
Note 1: 1C101 includes:
Opomba 1: Točka 1C101 vključuje:
Structural materials and coatings specially designed for reduced radar reflectivity;
strukturne materiale in prevleke, izdelane posebej za zmanjševanje radarske odbojnosti;
Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.
prevleke, vključno z barvami, izdelane posebej za zmanjševanje ali prikrojevanje odbojnosti ali oddajnosti v mikrovalovnem, infrardečem ali ultravijoličnem področju elektromagnetnega spektra.
Note 2: 1C101 does not include coatings when specially used for the thermal control of satellites.
Opomba 2: Točka 1C101 ne vključuje prevlek, kadar se uporabljajo za toplotni nadzor satelitov.
Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Ponovno nasičeni pirolizirani ogljiko-ogljikovi materiali, izdelani za vesoljska plovila iz točke 9A004 ali za sondirne rakete iz točke 9A104.
Graphite and ceramic materials, other than those specified in 1C007, as follows:
Grafit in keramični materiali, razen tistih iz točke 1C007:
Fine grain recrystallised bulk graphites having a bulk density of 1,72 g/cm3 or greater, measured at 288 K (15 °C), and having a particle size of 100 micrometres or less, usable for "missile" nozzles and re-entry vehicle nose tips, as follows:
drobnozrnati rekristalizirani grafit z gostoto 1,72 g/cm3 ali več, merjeno pri 288 K (15 °C), katerega delci merijo 100 mikrometrov ali manj, uporabni za "projektilne" dulce in obloge konic letal, ki se vračajo v ozračje, kakor sledi:
Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;
Valji premera 120 mm ali več in dolžine 50 mm ali več;
Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater;
Cevi z notranjim premerom 65 mm ali več in debelino stene 25 mm ali več, dolge 50 mm ali več;
Blocks having a size of 120 mm × 120 mm × 50 mm or greater;
Kocke velikosti 120 mm × 120 mm × 50 mm ali več;
N.B.: See also 0C004
NAPOTILO: Glej tudi točko 0C004.
Pyrolytic or fibrous reinforced graphites, usable for "missile" nozzles and re-entry vehicle nose tips;
pirolitsko ali z vlakni ojačani grafit, uporaben za "projektilne" dulce in obloge konic letal, ki se vračajo v ozračje;
Ceramic composite materials (dielectric constant less than 6 at frequencies from 100 Hz to 10000 MHz) usable for "missile" radomes;
keramični kompozitni materiali (z dielektrično konstanto manj kakor 6 pri frekvencah od 100 Hz do 10000 MHz), uporabni za ohišja "projektilov";
Bulk machinable silicon-carbide reinforced unfired ceramic, usable for "missile" nose tips.
keramika, ki je v masi ojačena s silicij-ogljikovimi vlakni, uporabna za konice "projektilov".
Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:
Goriva in sestavine goriv, razen tistih iz točke 1C011:
Propulsive substances:
pogonske snovi:
Spherical aluminium powder, other than that specified in the Military Goods Controls, with particles of uniform diameter of less than 200 μm and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591:1988 or national equivalents;
sferični aluminijev prah, razen tistega, ki je zajet v Nadzoru vojaškega blaga, z delci enakega premera, manjšega od 200 μm, in z vsebnostjo aluminija 97 ut. % ali več, če vsaj 10 ut.
A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).
Velikost delcev 63 μm (ISO R-565) ustreza 250 meshem (Tyler) ali 230 meshem (standard ASTM E-11).
Metal fuels, other than that specified in the Military Goods Controls, in particle sizes of less than 60 μm, whether spherical, atomized, spheroidal, flaked or ground, consisting 97 % by weight or more of any of the following:
kovinska goriva, razen tistih, ki so zajeta v nadzoru vojaškega blaga, z delci velikosti manj kakor 60 μm, bodisi sferičnimi, atomiziranimi, sferoidalnimi, v luskinah ali zmletimi, ki vsebujejo 97 ut:
Magnesium; or
magnezija; ali
Alloys of the metals specified by a. to c. above;
zlitin kovin iz zgornjih podtočk a. do c.;
Liquid oxidiser substances as follows:
tekoči oksidanti, kot so:
Dinitrogen trioxide;
didušikov trioksid;
Nitrogen dioxide/dinitrogen tetroxide;
dušikov dioksid/didušikov tetraoksid;
Dinitrogen pentoxide;
didušikov pentoksid;
Mixed Oxides of Nitrogen (MON);
mešani dušikovi oksidi (MON);
Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2) that can be used in missile systems.
Mešani dušikovi oksidi (MON) so raztopine dušikovega oksida (NO) v didušikovem tetraoksidu/dušikovem dioksidu (N2O4/NO2), ki se lahko uporabljajo v raketnih sistemih.
There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g., MON3 contains 3 % Nitric Oxide, MON25 25 % Nitric Oxide.
Obstaja vrsta koncentracij, ki se označijo kot MONi ali MONij, kjer sta i in j celi števili, ki predstavljata odstotek dušikovega oksida v mešanici (npr. MON3 vsebuje 3 % dušikovega oksida, MON25 pa 25 % dušikovega oksida.
An upper limit is MON40, 40 % by weight).
Zgornja meja je MON40, 40 mas. %).
SEE MILITARY GOODS CONTROLS FOR Inhibited Red Fuming Nitric Acid (IRFNA);
GLEJ NADZOR VOJAŠKEGA BLAGA ZA inhibirano rdečo kadečo dušikovo kislino (IRFNA)
SEE MILITARY GOODS CONTROLS AND 1C238 FOR Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen.
GLEJ NADZOR VOJAŠKEGA BLAGA IN 1C238 ZA spojine iz fluora in enega ali več drugih halogenov, kisika ali dušika
Polymeric substances:
polimerne snovi:
Carboxy-terminated polybutadiene (CTPB);
karboksi-terminirani polibutadien (CTPB);
Hydroxy-terminated polybutadiene (HTPB), other than that specified in the Military Goods Controls;
hidroksi-terminirani polibutadien (HTPB), razen tistega, ki je zajet v Nadzoru vojaškega blaga;
Polybutadiene-acrylic acid (PBAA);
polibutadien-akrilna kislina (PBAA);
Polybutadiene-acrylic acid-acrylonitrile (PBAN);
polibutadien-akrilnokislinski akrilonitril (PBAN);
Other propellant additives and agents:
drugi pogonski aditivi in agenti:
SEE MILITARY GOODS CONTROLS FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;
GLEJ NADZOR VOJAŠKEGA BLAGA ZA Karborani, dekaborani, pentaborani in njihovi derivati;
Triethylene glycol dinitrate (TEGDN);
trietilen-glikol dinitrat (TEGDN);
2-Nitrodiphenylamine;
2-nitrodifenilamin;
Trimethylolethane trinitrate (TMETN);
trimetiloletan trinitrat (TMETN);
Diethylene glycol dinitrate (DEGDN);
dietilen-glikol dinitrat (DEGDN);
Ferrocene derivatives as follows:
Derivati ferocena:
See Military Goods Controls for catocene;
Glej nadzor vojaškega blaga za katocen;
Ethyl ferrocene;
etil-ferocen;
Propyl ferrocene;
propil-ferocen;
See Military Goods Controls for n-butyl ferrocene;
Glej nadzor vojaškega blaga za n-butil ferocen;
Pentyl ferrocene;
pentil-ferocen;
Dicyclopentyl ferrocene;
pentil-ferocen;
Dicyclohexyl ferrocene;
dicikloheksil-ferocen;
Diethyl ferrocene;
dietil-ferocen;
i. Dipropyl ferrocene;
i. dipropil-ferocen;
Dibutyl ferrocene;
dibutil-ferocen;
Dihexyl ferrocene;
diheksil-ferocen;
Acetyl ferrocenes;
acetil-ferocen;
See Military Goods Controls for ferrocene Carboxylic acids;
Glej nadzor vojaškega blaga za ferocen-karboksilne kisline;
See Military Goods Controls for butacene;
Glej nadzor vojaškega blaga za butacen;
Other ferrocene derivatives usable as rocket propellant burning rate modifiers, other than those specified in the Military Goods Controls.
drugi derivati ferocena, uporabni za prilagajanje hitrosti gorenja raketnega goriva, razen tistih, ki so zajeti v Nadzoru vojaškega blaga.
Note: For propellants and constituent chemicals for propellants not specified in 1C111, see the Military Goods Controls.
Opomba: Glede goriv in sestavin goriv, ki niso zajeti v točki 1C111, glej Nadzor vojaškega blaga.
Maraging steels (steels generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce age-hardening) having an ultimate tensile strength of 1,500 MPa or greater, measured at 293 K (20 °C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm.
Martenzitna jekla (jekla, na splošno določena z visokim deležem niklja, zelo nizkim deležem ogljika in uporabo nadomestnih elementov ali usedlin, ki omogočajo utrjevanje s staranjem) z natezno trdnostjo najmanj 1500 MPa ali več, merjeno pri 293 K (20 °C), in so v obliki pločevine, plošče ali cevi z debelino 5 mm ali manj.
N.B.: SEE ALSO 1C216.
NAPOTILO: GLEJ TUDI TOČKO 1C216.
Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97 % or greater for fabrication of "missile" motor components, i.e., heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces.
Volfram, molibden in njune zlitine v obliki enakih sferičnih ali atomiziranih delcev premera 500 mikrometrov ali manj, čistote 97 % ali več, ki se uporabljajo za izdelavo elementov motorjev za "rakete", to je za toplotne ščite, podlage za dulce, vratove dulcev in površine, ki se uporabljajo za krmiljenje potiska.
Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:
Dvojno nerjaveče jeklo, stabilizirano s titanom (Ti-DSS):
Having all of the following characteristics:
ima vse naslednje značilnosti:
Containing 17,0-23,0 weight percent chromium and 4,5-7,0 weight percent nickel;
vsebuje 17,0 do 23,0 ut. % kroma in 4,5 do 7,0 ut. % niklja;
Having a titanium content of greater than 0,10 weight percent; and
vsebuje več kakor 0,10 ut. % titana; in
A ferritic-austenitic microstructure (also referred to as a two-phase microstructure ) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); and
ima feritno-avstenitno mikrostrukturo (imenovano tudi dvofazna mikrostruktura), ki je najmanj 10 vol. % avstenitna (merjeno po ASTM E-1181-87 ali enakovrednem nacionalnem postopku); in
Having any of the following forms:
ki ima katero koli od naslednjih oblik:
Ingots or bars having a size of 100 mm or more in each dimension;
ingoti ali palice, pri katerih je vsaka dimenzija enaka ali večja 100 mm;
Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or
listi širine 600 mm ali več in debeline 3 mm ali manj; ali
Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.
cevi z zunanjim premerom 600 mm ali več in debelino sten 3 mm ali manj.
Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:
Naslednje zlitine, razen tistih, določenih v točki 1C002.b.3. ali b.4:
Aluminium alloys having both of the following characteristics:
aluminijeve zlitine, ki imajo obe naslednji značilnosti:
'Capable of' an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and
natezno trdnost 460 MPa ali več pri 293 K (20 °C); in
In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;
obliko cevi ali trdno valjasto obliko (vključno z odkovki) z zunanjim premerom, ki je večji od 75 mm;
Titanium alloys having both of the following characteristics:
titanove zlitine, ki imajo obe naslednji značilnosti:
'Capable of' an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and
natezno trdnost 900 MPa ali več pri 293 K (20 °C); in
In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.
obliko cevi ali trdno valjasto obliko (vključno z odkovki) z zunanjim premerom, ki je večji od 75 mm;
The phrase alloys 'capable of' encompasses alloys before or after heat treatment.
Zgoraj navedene zlitine se nanašajo na zlitine pred toplotno obdelavo ali po njej.
'Fibrous or filamentary materials' or prepregs, other than those specified in 1C010.a., b. or e., as follows:
"Vlakneni ali nitasti materiali" ali prepregi, razen tistih, ki so določeni v točkah 1C010.a, b ali e:
Carbon or aramid 'fibrous or filamentary materials' having either of the following characteristics:
ogljikovi ali aramidni "vlakneni ali nitasti materiali", ki imajo eno od naslednjih značilnosti:
A "specific modulus" of 12,7 × 106 m or greater; or
"specifični modul" 12,7 × 106 m ali več; ali
A "specific tensile strength" of 235 × 103 m or greater;
"specifično natezno trdnost", 235 × 103 m ali več;
Note: 1C210.a. does not control aramid 'fibrous or filamentary materials' having 0,25 percent or more by weight of an ester based fibre surface modifier;
Opomba: Točka 1C210.a ne zajema aramidnih ”vlaknenih ali nitastih materialov”, v katerih je masni delež na estrih baziranih sredstev za površinsko spremembo vlaken 0,25 % ali več;
Glass 'fibrous or filamentary materials' having both of the following characteristics:
stekleni "vlakneni ali nitasti materiali", ki imajo obe naslednji značilnosti:
A "specific modulus" of 3,18 × 106 m or greater; and
"specifični modul" 3,18 × 106 m ali več; in
A "specific tensile strength" of 76,2 × 103 m or greater;
"specifično natezno trdnost", 76,2 × 103 m ali več;