Performance Assessment of Fuels TMEDA-DMAZ and Tonka۲۵۰ with Liquid Oxidizer AK۲۷

سال انتشار: 1402
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 32

فایل این مقاله در 8 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

JR_IJCCE-42-2_013

تاریخ نمایه سازی: 17 خرداد 1404

چکیده مقاله:

Tonka۲۵۰ is a liquid fuel containing equal percentages of triethylamine and xylidine which has attracted the attention of space industries due to its favorable performance characteristics. Tonka۲۵۰ has a low Ignition Delay (ID) time in the presence of AK۲۷ as a liquid oxidizer (about ۲۴ ms) and can be used as a starter fuel in engines working with a non-hypergolic combination of fuels and oxidizers. In recent years, due to the carcinogenic effect of Tonka۲۵۰, novel fuels have been introduced to replace it with high-performance properties and non-carcinogenic effects. A combination of tetramethyl ethylene diamine (TMEDA) and dimethyl aminoethyl azide (DMAZ) can be a candidate for this purpose. According to the results obtained from the current research, the equal weight percentage of TMEDA and DMAZ has an ID time of ۱۴ ms in reaction with AK۲۷. The ID time was measured through the cup test method with a fuel droplet in the liquid oxidizer. The density and density specific impulse of fuel TMEDA-DMAZ are close to those for Tonka۲۵۰ while the values of specific impulse for fuel TMEDA-DMAZ are about ۶ seconds more favorable than Tonka۲۵۰ at the chamber and exit pressures ۶.۸ MPa and ۰.۱ MPa, respectively. Therefore, it seems that fuel TMEDA-DMAZ is a good candidate for replacement for Tonka۲۵۰.

نویسندگان

Hossein Rouhandeh

Faculty of Chemistry & Chemical Engineering, Malek Ashtar University of Technology, P.O. Box: ۱۶۷۶۵/۳۴۵۴ Tehran, I.R. IRAN

Shahram Ghanbari Pakdehi

Faculty of Chemistry & Chemical Engineering, Malek Ashtar University of Technology, P.O. Box: ۱۶۷۶۵/۳۴۵۴ Tehran, I.R. IRAN

Mohammad Mahdi Bahri Rashabadi

Faculty of Chemistry & Chemical Engineering, Malek Ashtar University of Technology, P.O. Box: ۱۶۷۶۵/۳۴۵۴ Tehran, I.R. IRAN

Esmaeil Valizadeh

Faculty of Chemistry & Chemical Engineering, Malek Ashtar University of Technology, P.O. Box: ۱۶۷۶۵/۳۴۵۴ Tehran, I.R. IRAN

مراجع و منابع این مقاله:

لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :
  • Sutton G.P., "History of Liquid Propellant Rocket Engine", AIAA, New ...
  • Oefelein J.C., Yang V., Comprehensive Review of Liquid-Propellant Combustion Instabilities ...
  • Crocco L., Aspects of Combustion Stability in Liquid Propellant Rocket ...
  • Lee T.H., Lee C.H., Review of the Liquid Propulsion Technology, ...
  • Nie Y., Cheng Y., Wu J., Liquid-Propellant Rocket Engine Online ...
  • Altman D., Carter J.M., Penner S.S., Summerfield M., "Liquid Propellant ...
  • Bhosale V.K., Kulkarni S.G., Kulkarni P.S., Theoretical Performance Evaluation of ...
  • Gupta B.L., Varma M., Ignition and Combustion Studies on Metallized ...
  • Jyoti B.V.S., Naseem M.S., Baek S.W., Hypergolicity and Ignition Delay ...
  • Isaac Sam I., Gayathri S., Santhosh G., Cyriac J., Reshmi ...
  • Belal H., Ah El-S M., Al-Sanabawy M., Vaporization-Controlled Simplified Model ...
  • Soltani M., Ghorbanian K., Ashjaee M., Morad M., Spray Characteristics ...
  • Elnaggar A., Belal H., EL-Senbawi M.A., Feasibility Study and Modeling ...
  • Clark J.D., "Ignition!", Rutgers University Press, New Jersey (۲۰۱۸) ...
  • Mahyari M.N., Karimi H., Naseh H., Mirshams M., Numerical and ...
  • Thompson D.M., Tertiary Amine Azides in Hypergolic Liquid or Gel ...
  • Kandhakumar G., Kalaiarasi C., Kumaradhas P., Structure and Charge Density ...
  • Yu J., Baek S.W., Cho S.J., Experimental Study on Decomposition ...
  • Xie H., Mu X., Zhang Y., Wang X., Theory Investigation ...
  • Jain S.R., Self-Igniting Fuel-Oxidizer System and Hybrid Rocket, J. Sci. ...
  • Ghanbari Pakdehi S., Shirzadi B., Specific Impulse and Ignition Delay ...
  • Hollingshead J., Litzinger M., Kiaoulias D., Eckenrode L., Moore J.D., ...
  • Wang S., Thynell S.T., "Decomposition and Combustion of Ionic Liquid ...
  • Kurilov M., Kirchberger C.U., Freudenmann D., Stiefel A.D., Ciezki H.K., ...
  • Sutton G.P., Biblarz O., "Rocket Propulsion Elements", John Wiley & ...
  • Bibin C., Devan P.K., Kumar S.S., Gopinath S., Sheeja R., ...
  • Sai Kiran S., Madhu S., Bibin C., Woldegiorgis M.M., Kumran ...
  • Bibin C., Gopinath S., Aravindraj R., Devaraj A., Krishnan S.G., ...
  • Bibin C., Seenikannan P., Devan P.K., Performance, Emission, and Combustion ...
  • Bibin C., Kannan P.S., Devan P.K., Rajesh R., Performance and ...
  • Soundararajan G., Kumarasami D.P., Bibin C., Viswanathan P.K., Influence of ...
  • Hein M., Arena S., Willard C., "Foundations of College Chemistry", ...
  • Saksena P., "Study of Condensed Phase Reactions Between Hypergolic Propellants ...
  • Zhang P., Zhang L., Law C.K., Density Functional Theory Study ...
  • Ghanbari Pakdehi S., Shirzadi, B., The Effect of Some Amines ...
  • نمایش کامل مراجع