New solid propellants based on energetic binders and HNF

摘要: Abstract In view of Europe's need for more energetic as well clean storable solid rocket propellants, formulations based on ammonium nitrate (AN), dinitramine (ADN) and hydrazinium nitroformate (HNF) oxidizers, glycidyl azide polymer (GAP), polyglycidyl (PGN), polynitromethyloxetane (PLN) 3,3-bis(azydomethyl)oxetane (BAMO) binders aluminum (A1) an additional fuel are looking promising in terms theoretical performance. These propellant do not contain chlorine or compounds are, compared to conventional perchlorate (AP) with respect environmental aspects virtually non-polluting. For a number oxidizer combinations performance figures given various oxidizer-to-fuel (O/F) ratios using the content parameter. Performance show that combination HNF/A1/GAP, particular, is very one. The ingredients HNF GAP were synthesized small quantities their relevant properties determined. A high HNF/A1/GAP formulation was characterized tested laboratorium scale burner yielding pressure vs burning rate data.