(10) DIPAM (3,3′‑Diamino‑2,2′,4,4′,6,6′‑hexanitrobiphenyl or dipicramide) (CAS 17215–44–0);
(11) DNAN (2,4‑Dinitroanisole) (CAS 119‑27‑7);
(12) DNGU (DINGU or dinitroglycoluril) (CAS 55510–04–8);
(13) furazans, as follows:
(i) DAAOF (DAAF. DAAFox or diaminoazoxyfurazan);
(ii) DAAzF (diaminoazofurazan) (CAS 78644–90–3);
(iii) ANF (Furazanamine, 4‑nitro‑ or 3‑Amino‑4‑nitrofurazan; or 4‑Nitro‑1,2,5‑oxadiazol‑3‑amine; or 4‑Nitro‑3‑furazanamine; CAS 66328‑69‑6);
(iv) ANAzF (Aminonitroazofurazan or 1,2,5‑Oxadiazol‑3‑amine, 4‑[2‑(4‑nitro‑1,2,5‑oxadiazol‑3‑yl) diazenyl]; or 1,2,5‑Oxadiazol‑3‑amine, 4‑[(4‑nitro‑1,2,5‑oxadiazol‑3‑yl)azo]‑ (9CI); or Furazanamine, 4‑[(nitrofurananyl)azo]‑; or 4‑[(4‑Nitro‑1,2,5‑oxadiazol‑3‑yl)azo]‑1,2,5‑oxadiazol‑3‑amine) (CAS 155438‑11‑2);
(37) energetic ionic materials melting between 343 K (70°C) and 373 K (100°C) and with detonation velocity exceeding 6800 m/s or detonation pressure exceeding 18 GPa (180 kbar);
(38) explosives not listed elsewhere in paragraph (a) with a detonation velocity exceeding 8,700m/s at maximum density or a detonation pressure exceeding 34 Gpa (340 kbar).
(b) Propellants, as follows (MT for composite and composite modified double‑base propellants):
(1) any solid propellant with a theoretical specific impulse (see paragraph (k)(4)) greater than:
(i) 240 seconds for non‑metallised, non‑halogenated propellant;
(ii) 250 seconds for non‑metallised, halogenated propellant;
(iii) 260 seconds for metallised propellant;
(2) propellants having a force constant of more than 1,200 kJ/kg;
(3) propellants that can sustain a steady‑state burning rate more than 38mm/s under standard conditions (as measured in the form of an inhibited single strand) of 6.89 Mpa (68.9 bar) pressure and 294K (21°C);
(4) elastomer modified cast double based propellants with extensibility at maximum stress greater than 5% at 233 K (−40C);
(5) other composite and composite modified double‑base propellants;
(c) Pyrotechnics, fuels and related substances, and mixtures thereof:
(1) alane (aluminum hydride)(CAS 7784–21–6);
(2) carboranes; decaborane (CAS 17702–41–9); pentaborane and derivatives thereof (MT);
(3) liquid high energy density fuels, as follows (MT):
(i) mixed fuels that incorporate both solid and liquid fuels, such as boron slurry, having a mass‑based energy density of 40 MJ/kg or greater;
(ii) other high energy density fuels and fuel additives (for example, cubane, ionic solutions, JP‑7, JP‑10) having a volume‑based energy density of 37.5 GJ per cubic metre or greater, measured at 20°C and one atmosphere (101.325 kPa) pressure;
(4) metal fuels, and fuel or pyrotechnic mixtures, in particle form whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99% or more of any of the following:
(i) metals and mixtures thereof, as follows:
(A) beryllium (CAS 7440–41–7) in particle sizes of less than 60 micrometres (MT);
(B) iron powder (CAS 7439–89–6) with particle size of 3 micrometres or less produced by reduction of iron oxide with hydrogen;
(ii) fuel mixtures of pyrotechnic mixtures, which contain any of the following:
(A) boron (CAS 7440–42–8) or boron carbide (CAS 12069–32–8) fuels of 85% purity or higher and particle sizes of less than 60 micrometres;
(B) zirconium (CAS 7440–67–7), magnesium (CAS 7439–95–4) or alloys of these in particle sizes of less than 60 micrometres;
(iii) explosives and fuels containing the metals or alloys listed in subparagraphs (c)(4)(i) and (ii) whether or not the metals or alloys are encapsulated in aluminum, magnesium, zirconium, or beryllium;
(5) fuel, pyrotechnic, or energetic mixtures having any nanosized aluminium, beryllium, boron, zirconium, magnesium, or titanium, as follows:
(i) having particle size less than 200 nm in any direction;
(ii) having 60% or higher purity;
(6) pyrotechnic and pyrophoric materials, as follows:
(i) pytrotechnic or pyrophoric materials specifically formulated to enhance or control the production of radiated energy in any part of the IR spectrum;
(ii) mixtures of magnesium, polytetrafluoroethylene and the copolymer vinylidene difluoride and hexafluoropropylene (MT);
(7) titanium subhydride (TiHn) of stoichiometry equivalent to n = 0.65–1.68;
(8) hydrocarbon fuels specially formulated for use in flame throwers or incendiary munitions containing metal stearates (for example, octal) or palmitates, and M1, M2 and M3 thickeners.
Note: Subsubparagraph (3)(ii)—JP‑4, JP‑8, fossil refined fuels or biofuels, or fuels for engines certified for use in civil aviation are not included.
(d) Oxidizers, as follows:
(1) ADN (ammonium dinitramide or SR–12) (CAS 140456–78–6) (MT);
(2) AP (ammonium perchlorate) (CAS 7790–98–9) (MT);
(10) inhibited red fuming nitric acid (IRFNA) (CAS 8007–58–7) and liquid oxidisers comprised of or containing IRFNA or oxygen difluoride (MT for liquid oxidisers comprised of IRFNA);
(11) perchlorates, chlorates, and chromates composited with powdered metal or other high energy fuel components controlled under this category (MT).
(e) Binders, and mixtures thereof, as follows:
(1) AMMO (azidomethylmethyloxetane and its polymers) (CAS 90683–29–7);
(2) BAMO 3‑3 (bis(azidomethyl)oxetane and its polymers) (CAS 17607–20–4);
(6) GAP (glycidyl azide polymer) (CAS 143178–24–9) and its derivatives (MT for GAP);
(7) HTPB (hydroxyl‑terminated polybutadiene) with a hydroxyl functionality equal to or greater than 2.2 and less than or equal to 2.4, a hydroxyl value of less than 0.77 meq/g, and a viscosity at 30 °C of less than 47 poise (CAS 69102–90–5) (MT);
(xv) other ferrocene derivatives that do not contain a six carbon aromatic functional group attached to the ferrocene molecule (MT if usable as rocket propellant burning rate modifier);
(5) lead beta‑resorcylate (CAS 20936–32–7);
(6) lead citrate (CAS 14450–60–3);
(7) lead‑copper chelates of beta‑resorcylate or salicylates (CAS 68411–07–4);
(8) lead maleate (CAS 19136–34–6);
(9) lead salicylate (CAS 15748–73–9);
(10) lead stannate (CAS 12036–31–6);
(11) MAPO (tris‑1‑(2‑methyl)aziridinyl phosphine oxide) (CAS 57–39–6); BOBBA–8 (bis(2‑methyl aziridinyl) 2‑(2‑hydroxypropanoxy) propylamino phosphine oxide); and other MAPO derivatives (MT for MAPO);
(i) neopentyl[diallyl]oxy, tri [dioctyl] phosphatotitanate (CAS 103850–22–2); also known as titanium IV, 2,2[bis 2‑propenolato‑methyl, butanolato, tris (dioctyl) phosphato] (CAS 110438–25–0), or LICA 12 (CAS 103850–22–2);
(ii) titanium IV, [(2‑propenolato‑1) methyl, n‑propanolatomethyl] butanolato‑1, tris(dioctyl)pyrophosphate, or KR3538;
(iii) titanium IV, [2‑propenolato‑1)methyl, propanolatomethyl] butanolato‑1, tris(dioctyl) phosphate;
(ii) polyfunctional aziridine amides with isophthalic, trimesic, isocyanuric, or trimethyladipic backbone also having a 2‑methyl or 2‑ethyl aziridine group;
(17) superfine iron oxide (Fe2O3, hematite) with a specific surface area more than 250 m2/g and an average particle size of 0.003 micrometres or less (CAS 1309–37–1);
(18) TEPAN (HX‑879) (tetraethylenepentaamineacrylonitrile) (CAS 68412–45–3); cyanoethylated polyamines and their salts (MT for TEPAN (HX‑879);
(19) TEPANOL (HX‑878) (Tetraethylenepentaamineacrylo‑nitrileglycidol) (CAS 68412–46–4); cyanoethylated polyamines adducted with glycidol and their salts (MT for TEPANOL (HX‑878);
(20) TPB (triphenyl bismuth) (CAS 603–33–8) (MT);
(21) Tris (ethoxyphenyl) bismuth (TEPB) (CAS 90591‑48‑3).
Note: Subsubparagraph (16)(ii)—included are:
(a) 1,1H‑Isophthaloyl‑bis(2‑methylaziridine) (HX‑752) (CAS 7652‑64‑4); and
(b) 2,4,6‑tris(2‑ethyl‑1‑aziridinyl)‑1,3,5‑triazine (HX‑874) (CAS 18924‑91‑9); and
(h) Any explosive, propellant, pyrotechnic, fuel, oxidiser, binder, additive, or precursor that (MT for articles designated as such):
(1) is classified; or
(2) is being developed using classified information.
(i) Developmental explosives, propellants, pyrotechnics, fuels, oxidisers, binders, additives, or precursors therefor funded by the United States Government via contract or other funding authorisation.
Note 1: This paragraph does not control explosives, propellants, pyrotechnics, fuels, oxidisers, binders, additives, or precursors therefor:
(b) identified in the relevant United States Government contract or other funding authorisation as being developed for both civil and military applications.
Note 2: Note 1 does not apply to defence articles enumerated on this list, whether in production or development.
Note 3: This paragraph applies only to those contracts and funding authorisations that are dated 5 January 2015, or later.
(j) Technical data and defence services directly related to the defence articles described in paragraphs (a) to (i) (MT for articles designated as such).
(k) The following interpretations explain and amplify the terms used in this category and elsewhere in this list:
(1) Category V contains explosives, energetic materials, propellants and pyrotechnics and specially formulated fuels for aircraft, missile and naval applications. Explosives are solid, liquid or gaseous substances or mixtures of substances, which, in their primary, booster or main charges in warheads, demolition or other military applications, are required to detonate;
(2) the resulting product of the combination or conversion of any substance controlled by this category into an item not controlled will no longer be controlled by this category provided the controlled item cannot easily be recovered through dissolution, melting, sieving, etc. As an example, beryllium converted to a near net shape using hot isostatic processes will result in an uncontrolled part. A cured thermoset containing beryllium powder is not controlled unless meeting an explosive or propellant control. The mixture of beryllium powder in a cured thermoset shape is not controlled by this category. The mixture of controlled beryllium powder mixed with a typical propellant binder will remain controlled by this category. The addition of dry silica powder to dry beryllium powder will remain controlled;
(3) subparagraph (c)(4)(ii)(A) does not apply to boron and boron carbide enriched with boron‑10 (20% or more of total boron‑10 content;
(4) theoretical specific impulse (Isp) is calculated using standard conditions (1000 psi chamber pressure expanded to 14.7 psi) and measured in units of pound‑force‑seconds per pound‑mass (lbf‑s/lbm) or simplified to seconds (s). Calculations will be based on shifting equilibrium;
(5) particle size is the mean particle diameter on a weight basis. Best industrial practices will be used in determining particle size and the controls may not be undermined by addition of larger or smaller sized material to shift the mean diameter;
(l)‑(w) [Reserved]
Note: Use of this paragraph is limited to exports of defence articles controlled in this category where the purchase documentation includes commodities, software, or technical data.
Note 1: To assist the exporter, an item has been categorised by the most common use. Also, where appropriate, references have been provided to the related controlled precursors.
Note 2: Chemical Abstract Service (CAS) registry numbers do not cover all the substances and mixtures controlled by this category. The numbers are provided as examples to assist the government agencies in the license review process and the exporter when completing their licence application and export documentation.