natgillin/translations-raw huggingface dataset:
a pour point at 219 K (–54 °C) or less;
točka litja pri 219 K (–54 °C) ali manj;
a viscosity index of 80 or more; and
indeks viskoznosti 80 ali več; in
a boiling point at 473 K (200 °C) or higher;
z vreliščem pri 473 K (200 °C) ali več;
lubricating materials containing, as their principal ingredients, any of the following compounds or materials:
maziva, katerih osnovna sestavina je katera koli od naslednjih spojin ali materialov:
phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or
fenilenovi ali alkilfenilenovi estri ali tioetri ali njihove mešanice, ki vsebujejo več kot dve etrski ali tioetrski funkciji ali njune mešanice; ali
fluorinated silicone fluids with a kinematic viscosity of less than 5000 mm2/s (5000 centistokes) measured at 298 K (25 °C);
tekočine iz fluoriranih silikonov s kinematično viskoznostjo manj kot 5000 mm2/s, merjeno pri 298 K (25 °C);
damping or flotation fluids with a purity exceeding 99,8 %, containing less than 25 particles of 200 μm or larger in size per 100 ml and made from at least 85 % of any of the following compounds or materials:
tekočine za dušenje ali flotacijo s čistoto več kot 99,8 %, ki vsebujejo manj kot 25 delcev, velikih 200 μm ali večjih na 100 ml, in ki vsebujejo najmanj 85 % katere koli od naslednjih spojin ali materialov:
dibromotetrafluoroethane;
dibromotetrafluoretana;
polychlorotrifluoroethylene (oily and waxy modifications only); or
poliklortrifluoretilena (samo oljnih ali voskastih modifikacij); ali
polybromotrifluoroethylene;
polibromtrifluoretilena;
fluorocarbon electronic cooling fluids, having all of the following characteristics:
fluoroogljikove elektronske hladilne tekočine, ki imajo vse naslednje značilnosti:
containing 85 % by weight or more of any of the following, or mixtures thereof:
vsebujejo 85 ut. % ali več katere koli od naslednjih sestavin ali njihovih mešanic:
monomeric forms of perfluoropolyalkylether-triazines or perfluoroaliphatic-ethers;
monomernih oblik polifluoro-poliakrileter-triazinov ali perfluoralifatskih etrov;
perfluoroalkylamines;
perfluoroalkiminov;
perfluorocycloalkanes; or
perfluorocikloalkanov; ali
perfluoroalkanes;
perfluoroalkanov;
density at 298 K (25 °C) of 1,5 g/ml or more;
njihova gostota pri 298 K (25 °C) je 1,5 g/ml ali več;
in a liquid state at 273 K (0 °C); and
pri 273 K (0 °C) so v tekočem stanju; in
containing 60 % or more by weight of fluorine.
vsebujejo 60 ut. % ali več fluora.
clash 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 loss in weight of each ball is less than 10 mg/mm2 of ball surface;
izguba mase vsake kroglice je manjša od 10 mg/mm2 njene površine;
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
the total acid or base number is less than 0,40;
skupno kislinsko ali bazično število je manjše od 0,40;
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.
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;
Note:1C007.b. does not control abrasives.
Opomba:Predmet nadzora iz točke 1C007.b niso abrazivi.
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 ojačeni z vlakni, ki imajo vse naslednje značilnosti:
made from any of the following materials:
izdelani so iz katerega koli od naslednjih materialov:
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 × 103m;
ceramic-ceramic "composite" materials, with or without a continuous metallic phase, incorporating particles, whiskers or fibres, where carbides or nitrides of silicon, zirconium or boron form the "matrix";
keramično-keramični "kompozitni" materiali z nepretrgano kovinsko fazo ali brez nje, ki vsebujejo delce, laske ali vlakna, pri katerih tvorijo "matrika" silicijevi karbidi ali nitridi, cirkonij ali bor;
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:
polydiorganosilanes (for producing silicon carbide);
polidiorganosilani (za proizvodnjo silicijevega karbida);
polysilazanes (for producing silicon nitride);
polisilazani (za proizvodnjo silicijevega nitrida);
polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components);
polikarbosilani (za proizvodnjo keramike s silicijevimi, ogljikovimi in dušikovimi komponentami);
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:
Note:1C007.f. does not control "composites" containing fibres from these systems with a fibre tensile strength of less than 700 MPa at 1273 K (1000 °C) or fibre tensile creep resistance of more than 1 % creep strain at 100 MPa load and 1273 K (1000 °C) for 100 hours.
Opomba:Predmet nadzora točke 1C007.f niso "kompoziti", v katerih imajo filamenti teh sistemov natezno trdnost manjšo od 700 MPa pri 1273 K (1000 °C) ali ki imajo trajno natezno trdnost večjo od 1 % razteza pri obremenitvi 100 MPa in pri temperaturi 1273 K (1000 °C) v časovnem obsegu 100 ur.
bismaleimides;
bis-maleimidi;
aromatic polyamide-imides;
aromatski poliamid-imidi;
aromatic polyimides;
aromatski poliamidi;
aromatic polyetherimides having a glass transition temperature (Tg) exceeding 513 K (240 °C);
aromatski polieterimidi s točko posteklenitve (Tg), višjo od 513 K (240 °C);
Note 1:1C008.a. controls the substances in liquid or solid form, including resin, powder, pellet, film, sheet, tape or ribbon;
Opomba 1:Predmet nadzora točke 1C008.a so snovi v tekočem ali trdnem stanju, vključno s smolo, prahom, peleti, filmi, listi, trakovi ali pasovi;
Note 2:1C008.a. does not control non-fusible compression moulding powders or moulded forms.
Opomba 2:Predmet nadzora po točki 1C008.a niso netaljivi talilni prahi ali talilne oblike.
Thermoplastic liquid crystal copolymers having a heat distortion temperature exceeding 523 K (250 °C) measured according to ISO 75-2 (2004), method A or national equivalents, with a load of 1,80 N/mm2 and composed of:
termoplastični polimeri tekočih kristalov s točko temperaturne deformacije nad 523 K (250 °C), merjeno po ISO 75–2 (2004) ali po enakovrednih nacionalnih metodah, in z obremenitvijo 1,80 N/mm2, ki so sestavljeni:
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
any of the following acids:
iz katere koli od naslednjih kislin:
terephthalic acid;
tereftalne kisline;
not used;
se ne uporabljajo;
polyarylene ketones;
poliarilen ketoni;
polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;
poliarilen sulfidi, pri katerih je arilenska skupina bifenil, trifenil ali njuna kombinacija;
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.
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.
N.B.:SEE ALSO 1C210 AND 9C110.
NAPOTILO:GLEJ TUDI 1C210 IN 9C110.
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 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.
Inorganic "fibrous or filamentary materials", having all of the following:
organski "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 kot 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":
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;
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:
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.
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 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 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;
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:
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’, "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 ali "projektilov" ali zračna plovila brez posadke, določene v 9A012.
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.
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 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
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 rocket nozzles and re-entry 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.
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.
metal fuels, other than that specified in the Military Goods Controls, in particle sizes of less than 60 μm, whether spherical, atomised, 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:
zirconium;
cirkonija;
beryllium;
berilija;
magnesium; or
magnezija; ali
alloys of the metals specified by (a) to (c) above;
zlitin kovin iz zgornjih podtočk a. do c.;
Oxidiser substances usable in liquid propellant rocket engines as follows:
Oksidanti, uporabni v raketnih motorjih na tekoče-kapljevito gorivo:
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);
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
Hydrazine derivatives as follows:
derivati hidrazina:
trimethylhydrazine;
trimetilhidrazin;
tetramethylhydrazine;
tetrametilhidrazin;
N, N diallylhydrazine;
N,N dialilhidrazin;
allylhydrazine;
alilhidrazin;
ethylene dihydrazine;
etilen dihidrazin;
monomethylhydrazine dinitrate;
monometilhidrazin dinitrat;
unsymmetrical dimethylhydrazine nitrate;
nesimetrični dimetilhidrazin nitrat;
hydrazinium azide;
hidrazinijev azid;
i. dimethylhydrazinium azide;
i. dimetilhidrazinijev azid;