@techreport{oai:jaxa.repo.nii.ac.jp:00002004,
 author = {Fujisato, Koji and Habu, Hiroto and Hori, Keiichi and Shibamoto, Hidefumi and Yu, Xiuchao and Miyake, Atsumi and Fujisato, Koji and Habu, Hiroto and Hori, Keiichi and Shibamoto, Hidefumi and Yu, Xiuchao and Miyake, Atsumi},
 month = {Mar},
 note = {Combustion characteristics of pelletized ammonium dinitramide (ADN) and ADN-based propellants have been studied. Micron-meter-sized particles of Al, Fe2O3, TiO2, NiO, Cu(OH)NO3, Cu and CuO, and nano-meter-sized Al (Alex) and CuO (nanoCuO) were employed as the additives for pelletized ADN. Only nanoCuO and Alex show the remarkable effects, so they are also added to ADN-based propellant. The binder of ADN-based propellant is thermoplastic elastomer (TP), and three kinds of mixtures (TP:ADN = 30:70, 20:80 and 10:90 mass%) were prepared .The burning rates of pelletized ADN and ADN-based propellants were measured under the pressure range from 0.6 to 6.2 MPa, and the surface temperature profiles were obtained about ADN-based propellants. Nano-sized CuO enhanced the burning rate of pelletized ADN. Alex-incorporated ADN burned with flames even at 0.55 MPa under which pure ADN does not form the flame. Burning rate of nonadditive ADN-based propellants has extremely high pressure dependency. In the case of TP/ADN (30:7, burning rate jump are found from the critical pressure approximately 3.2MPa. The temperature profiles of TP/ADN (30:70) were measured, and the combustion　structure was discussed. Both nanoCuO and Alex improved the burning rate characteristics,　and the pressure exponents are 0.54 and 0.76 respectively., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061907001, レポート番号: JAXA-RR-12-005},
 title = {Combustion wave structure of ADN based composite propellant},
 year = {2013}
}