BALLISTIC SCALE-UP OF NF PROPELLANTS. I. 80 LBM MOTOR DEMONSTRATION FIRING,

Abstract

Production of an NFPA/TVOPA propellant having a new prepolymer binder system was scaled up from gram to multipound batches in six months. Ballistic scaling data on RH-SE-103cf were obtained in motors ranging in size from 10 grams to 80-lbm during this time. The burning rate was 0.97 in/sec at 1000 psia and the pressure exponent was 0.6. A specific impulse (Isps) of 261.3 lbf-sec/lbm (97% of theoretical) was obtained from the 80-lbm motor firing. The radar attenuation properties of RH-SE-103 (NF) and RH-P-112 (PNC) exhaust plumes were compared by measurements made about 1-ft and 5-ft from the nozzle exit planes. The X-band attenuation at the 1-ft measurement station was about 1.23 db for the high-energy NF propellant compared with 5.84 db for the PNC propellant. In a preliminary study of techniques for evaluating possible toxicity hazards, samples of exhaust gases from the 80-lbm motor were obtained for HF analysis using evacuated stainless-steel bottles. A polyester-based liner material which had been used with previous NF propellants was also satisfactory for the new system. Propellant would not bond well to fully-cured liner, but excellent bonds were obtained when the propellant was cast on partially-cured liner. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 17, 1966
Accession Number
AD0370635

Entities

People

  • S. E. Anderson

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Energy
  • Exhaust Gases
  • Exhaust Plumes
  • Frequency
  • Gases
  • High Energy
  • Materials
  • Measurement
  • Mechanical Properties
  • Production
  • Specific Impulse
  • Stainless Steel
  • Toxicity

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Rocket Propulsion.