natgillin/translations-raw huggingface dataset:
’Flash point’ is determined using the Cleveland Open Cup Method described in ASTM D-92 or national equivalents;
’plamenišče’ z uporabo metode Cleveland Open Cup, opisane v ASTM D-92, ali enakovrednih nacionalnih metod;
’Pour point’ is determined using the method described in ASTM D-97 or national equivalents;
’točka litja’ z uporabo metode, opisane v ASTM D-97, ali enakovrednih nacionalnih metod;
’Viscosity index’ is determined using the method described in ASTM D-2270 or national equivalents;
’indeks viskoznosti’ z uporabo metode, opisane v ASTM D-2270, ali enakovrednih nacionalnih metod;
’Thermal stability’ is determined by the following test procedure or national equivalents:
’termična stabilnost’ z naslednjim preizkusom ali enakovrednimi nacionalnimi preizkusi:
The chamber is purged with nitrogen, sealed at atmospheric pressure and the temperature raised to and maintained at 644 ± 6 K (371 ± 6 °C) for six hours;
Komoro očistimo z dušikom, zapremo pri atmosferskem tlaku, temperaturo pa povečujemo do 644 ± 6 K (371 ±6 °C) in ohranjamo šest ur pri tej temperaturi;
The change in original viscosity as determined at 311 K (38 °C) is less than 25 %; and
sprememba izvorne viskoznosti, kakor je določena pri 311 K (38 °C), je manjša od 25 % in
’Autogenous ignition’ temperature is determined using the method described in ASTM E-659 or national equivalents.
’temperatura samovžiga’ se določi z uporabo metode, opisane v ASTM E-659, ali z uporabo enakovrednih nacionalnih metod.
N.B.:SEE ALSO 1C107.
Opomba:GLEJ TUDI TOČKO 1C107.
Base materials of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5000 ppm, an average particle size equal to or less than 5 µm and no more than 10 % of the particles larger than 10 µm;
osnovni materiali iz samostojnih ali kompleksnih boridov titana, katerih skupna nečistota (brez namenoma dodatnih dodatkov) je manj kot 5000 ppm, povprečna velikost delcev enaka ali manjša od petih mikrometrov in pri katerih ni več kot 10 % delcev večjih od 10 mikrometrov;
Non-"composite" ceramic materials in crude or semi-fabricated form, composed of borides of titanium with a density of 98 % or more of the theoretical density;
keramični materiali, ki niso "kompozitni", v surovi ali polpredelani obliki, sestavljeni iz boridov titana z gostoto 98 % ali več teoretične gostote;
Ceramic-ceramic "composite" materials with a glass or oxide-"matrix" and reinforced with fibres having all of the following:
keramično-keramični "kompozitni" materiali s stekleno ali oksidno "matriko" in ojačani z vlakni, ki imajo vse naslednje značilnosti:
Si-Al-O-N; or
Si-Al-O–N ali
Si-O-N; and
Si-O–N in
Having a "specific tensile strength" exceeding 12,7 × 103m;
s "specifično natezno trdnostjo", večjo od 12,7 × 103 m;
Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in 1C007.c., as follows:
predhodniki materialov (tj. posebej zanje namenjeni polimerni ali kovinoorganski materiali) za proizvodnjo katere koli faze ali faz materialov, naštetih v točki 1C007(c):
Ceramic-ceramic "composite" materials with an oxide or glass "matrix" reinforced with continuous fibres from any of the following systems:
keramično-keramični "kompozitni" materiali s kisikovo ali stekleno "matriko", ki so ojačani s kontinuiranimi vlakni iz enega od naslednjih sistemov:
Al2O3; or
Al2O3ali
Non-fluorinated polymeric substances as follows:
Nefluorirane polimerne snovi:
Note:1C008.a. controls substances in liquid or solid "fusible" form, including resin, powder, pellet, film, sheet, tape or ribbon.
Opomba:Predmet nadzora iz točke 1C008.a so snovi v tekočem ali trdnem "taljivem" stanju, vključno s smolo, prahom, peleti, filmi, listi, trakovi ali pasovi;
non-"fusible" aromatic polyimides in film, sheet, tape or ribbon form, see 1A003.
Opomba:Za "netaljive"aromatske poliamide v obliki filma, listov, trakov ali pasov glej točko 1A003.
Phenylene, biphenylene or naphthalene; or
fenilena, bifenilena ali naftalena ali
Methyl, tertiary-butyl or phenyl substituted phenylene, biphenylene or naphthalene; and
metila, iz fenilena s substituiranim terciarnim butilom ali fenilom, iz bifenilena ali naftalena in
6-hydroxy-2 naphthoic acid; or
6-hidroksi-2-naftojske kisline ali
Polybiphenylenethersulphone having a ’glass transition temperature (Tg)’ exceeding 513 K (240 °C).
polibifenileneter sulfoni s ’točko posteklenitve (Tg)’ višjo od 513 K (240 °C).
The ’glass transition temperature (Tg)’ for 1C008 materials is determined using the method described in ISO 11357-2 (1999) or national equivalents.
’Točka posteklenitve (Tg)’ pri materialih iz točke 1C008 se določa z uporabo suhe metode, opisane v ISO 11357–2 (1999) ali enakovrednimi nacionalnimi standardi.
Unprocessed fluorinated compounds as follows:
Nepredelane fluorirane spojine:
"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 AND 9C110.
Opomba:GLEJ TUDI 1C210 IN 9C110.
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 trdnostjo", 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:
organski "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 "civil aircraft" structures or laminates, in which the size of individual sheets does not exceed 100 cm × 100 cm.
Opomba:Predmet nadzora iz točke 1C010(b) niso izdelki, izdelani iz "vlaknenih ali nitastih materialov", ki se uporabljajo pri popravilu delov "civilnih zrakoplovov" ali laminatov, če velikost posamezne plošče ne presega 100 cm × 100 cm.
Properties for materials described in 1C010.b. should be determined using SACMA recommended methods SRM 12 to 17, ISO 10618 (2004) 10.2.1 Method A or national equivalent tow tests and based on lot average.
Značilnosti materialov, opisanih v točki 1C010.b, se določajo z uporabo metod z oznakami SRM 12 do 17, ISO 10618 (2004) 10.2.1 metoda A, ki jih priporoča "Suppliers Advance Composite Materials Association" (SACMA) ali z uporabo enakovrednih nacionalnih nateznih preskusov, ki temeljijo na povprečju velikega števila vzorcev.
A "specific modulus" exceeding 2,54 × 106 m; and
"specifičnim modulom", večjim od 2,54 × 106 m, in
Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 % by weight or more silica, with a "specific modulus" of less than 10 × 106 m;
nekontinuirana, mnogofazna, polikristalinska aluminijeva vlakna, narezana ali v naključnem prepletu, ki vsebujejo 3 ut. % ali več silicija, in katerih "specifični modul" je manj kot 10 × 106 m;
"Fibrous or filamentary materials", having any of the following:
"vlakneni ali nitasti materiali", ki imajo vse naslednje značilnosti:
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 "mešana vlakna" z drugimi vlakni, naštetimi v točkah 1C010(a), 1C010(b) ali 1C010(c);
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", having all of the following:
iz organskih ali ogljikovih "vlaknenih ali nitastih materialov", ki imajo vse naslednje značilnosti:
A "specific tensile strength" exceeding 17,7 × 104 m;
"specifično natezno trdnostjo", večjo od 17,7 × 104 m;
A "specific modulus" exceeding 10,15 × 106 m;
"specifičnim modulom", večjim od 10,15 × 106 m;
Not specified in 1C010.a. or 1C010.b.; and
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:
Opomba:Predmet nadzora točke 1C010(e) niso:
Epoxy resin "matrix" impregnated carbon "fibrous or filamentary materials" (prepregs) for the repair of "civil aircraft" structures or laminates, in which the size of individual sheets of prepreg does not exceed 100 cm × 100 cm;
"vlakneni ali nitasti materiali", impregnirani z "matriko" epoksi smol (prepregi) ki se uporabljajo pri popravilu delov "civilnih zrakoplovov" ali laminatov, če velikost posamezne plošče ne presega 100 cm × 100 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 (Tg)’ for phenolic and epoxy resins is determined using the method described in ASTM D 4065 at a frequency of 1Hz and a heating rate of 2 K (°C) per minute using the dry method.
’Temperaturna točka posteklenitve (Tg)’ 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.
N.B.:SEE ALSO MILITARY GOODS CONTROLS and 1C111.
Opomba: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 thereof;
kovine z velikostjo delcev manj kot 60 µm, bodisi sferične, atomizirane, sferoidne, v kosmičih ali drobljene, izdelane iz materiala, ki vsebuje 99 % ali več cirkonija, magnezija ali njunih zlitin;
Note:The metals or alloys specified 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 specified 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.
Nitroguanidine (NQ) (CAS 556-88-7).
nitrogvanidin nitrat (NQ) (CAS 556–88–7).
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 kot 50 ut. % deleža plutonija z izotopskim številom 238;
Note:1C012.a. does not control:
Opomba:Predmet nadzora točke 1C012(a) niso:
"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 v točki 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’, "missile" subsystems or unmanned aerial vehicles specified in 9A012.
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’, podsistemih "projektilov" ali zračna plovila brez posadke določene v 9A012.
In 1C101 ’missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
V točki 1C101 pomeni izraz ’projektilih’ komponente raketnih sistemov in neimenovanih zrakoplovov z dosegom več od 300 km.
Fine grain graphites with a bulk density of 1,72 g/cm3 or greater, measured at 288 K (15 °C), and having a grain size of 100 µm or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:
drobnozrnati grafit z gostoto 1,72 g/cm3 ali več, merjeno pri 288 K (15 °C), katerega delci merijo 100 µm ali manj, uporabni za raketne dulce (šobe) in obloge konic letal, ki se lahko obdelajo v katerega koli od naslednjih proizvodov:
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; or
cevi z notranjim premerom 65 mm ali več in debelino stene 25 mm ali več, dolge 50 mm ali več, ali
N.B.:SEE ALSO 0C004
Opomba:Glej tudi točko 0C004.
Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
pirolitsko ali z vlakni ojačani grafit, uporaben za raketne dulce (šobe) in konice letal, ki ponovno vstopajo v ozračje in so uporabni v "projektilih", vesoljska plovila iz točke 9A004 ali sondirne rakete iz točke 9A104;
Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
keramični kompozitni materiali (z dielektrično konstanto manj kot 6 pri frekvencah od 100 MHz do 100 GHz) za uporabo v kupolah radarskih anten, uporabnih v "projektilih", nosilnih raketah iz točke 9A004 ali sondirnih raketah iz točke 9A104.
Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
keramika, ki je v masi ojačana s silicij-ogljikovimi vlakni, uporabna za konice, uporabne v "projektilih", nosilnih raketah iz točke 9A004 ali sondirnih raketah iz točke 9A104;
Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
keramični kompozitni materiali, ojačani s silicij-ogljikovimi vlakni, uporabni za konice, letala, ki se vračajo v ozračje, in lopute šob, uporabne v "projektilih", nosilnih raketah iz točke 9A004 ali sondirnih raketah iz točke 9A104.
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 kot 60 µm, bodisi sferičnimi, atomiziranimi, sferoidalnimi, v luskinah ali zmletimi, ki vsebujejo 97 ut. % ali več katere koli od naslednjih snovi::
Alloys of the metals specified in a. to c. above;
zlitin kovin iz zgornjih podtočk (a) do (c);
Dinitrogen trioxide (CAS 10544-73-7);
didušikov trioksid (CAS 10544–73–7);
Nitrogen dioxide (CAS 10102-44-0)/dinitrogen tetroxide (CAS 10544-72-6);
dušikov dioksid (CAS 10102–44–0)/didušikov tetraoksid (CAS 10544–72–56);
Dinitrogen pentoxide (CAS 10102-03-1);
didušikov pentoksid (CAS 10102–03–1);
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;
Trimethylhydrazine (CAS 1741-01-1);
trimetilhidrazin (CAS 1741–01–1);
Tetramethylhydrazine (CAS 6415-12-9);
trimetilhidrazin (CAS 6415–12–9);
Allylhydrazine (CAS 7422-78-8);
alilhidrazin (CAS 7422–78–8);
Hydrazinium azide (CAS 14546-44-2);
hidrazinijev azid (CAS 14546–44–2);
i. Dimethylhydrazinium azide;
dimetilhidrazinijev azid;
Hydrazinium dinitrate;
hidrazinijev dinitrat;
Diimido oxalic acid dihydrazine;
diimido dihidrazin oksalne kisline;
See Military Goods Controls for Hydrazinium perchlorate;
Glej nadzor vojaškega blaga za hidrazinijev perklorat;
Hydrazinium diperchlorate;
hidrazinijev diperklorat;
Methylhydrazine nitrate (MHN);
metilhidrazin nitrat (MHN);
Carboxy-terminated polybutadiene (including carboxyl-terminated polybutadiene) (CTPB);
karboksi-terminirani polibutadien (vključno s karboksil-terminiranim polibutadienom) (CTPB);
Hydroxy-terminated polybutadiene (included hydroxyl-terminated polybutadiene) (HTPB), other than that specified in the Military Goods Controls;
hidroksi-terminirani polibutadien (vključno s hidroksil-terminiranim polibutadienom) (HTPB), razen tistega, ki je zajet v Nadzoru vojaškega blaga;
SEE MILITARY GOODS CONTROLS FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;
GLEJ NADZOR VOJAŠKEGA BLAGA ZA karborane, dekarborane, pentaborane in njihove derivate;
Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8);
trietilen-glikol dinitrat (TEGDN) (CAS 111–22–8);
2-Nitrodiphenylamine (CAS 119-75-5);
2-nitrodifenilamin (CAS 119–75–5);
Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);
trimetiloletan trinitrat (TMETN) (CAS 3032–55–1);
Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0);
dietilen-glikol dinitrat (DEGDN)(CAS 693–21–0);
Ethyl ferrocene (CAS 1273-89-8);
propil-ferocen (CAS 1273–89–8);
Pentyl ferrocene (CAS 1274-00-6);
pentil-ferocen (CAS 1274–00–6);
i. Dipropyl ferrocene;
dipropil-ferocen;
Dibutyl ferrocene (CAS 1274-08-4);
dibutil-ferocen (CAS 1274–08–4);
Dihexyl ferrocene (CAS 93894-59-8);
diheksil-ferocen (CAS 93894–59–8);
4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR), other than that specified in the Military Goods Controls.
4,5 diazidometil-2-metil-1,2,3-triazol (iso- DAMTR), razen tistih, določenih 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.
N.B.:SEE ALSO 1C216.
Opomba: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 rocket motor components usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 (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 raketnih motorjev, uporabnih v "projektilih", vesoljskih plovilih iz točke 9A004 ali sondirnih raketah iz točke 9A104 (tj. za toplotne ščite, podlage za dulce, vratove dulcev in površine, ki se uporabljajo za krmiljenje potiska).
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;
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
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
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:
’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
’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
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
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:Predmet nadzora točke 1C210.a niso aramidni ’vlakneni ali nitasti materiali’, 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
Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass ’fibrous or filamentary materials’ specified in 1C210.a. or b.
"preja", "predpreja", "predivo" ali "trakovi", impregnirani s smolo, ki so široki 15 mm ali manj (prepregi), izdelani iz ogljikovih ali steklenih ’vlaknenih ali nitastih materialov’, določenih v točki 1C210(a) ali (b)
Note:In 1C210, ’fibrous or filamentary materials’ is restricted to continuous "monofilaments", "yarns", "rovings", "tows" or "tapes".
Opomba:V točki 1C210 so ’vlakneni ali nitasti materiali’ omejeni na neskončno "monofilamentno prejo", "prejo", "predprejo", "predivo" ali "trakove".