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Infrared signature of NEPE, HTPB rocket plume under varying flight conditions and motor size

  • Published:2021-01 Issue: Volume:112 Page:103590
  • ISSN:1350-4495
  • Container-title:Infrared Physics & Technology
  • language:en
  • Short-container-title:Infrared Physics & Technology

Author:

Kim Sangmin,Kim Sanghoon,Kim Mintaek,Song Soonho,Lee Joon Sang

Publisher

Elsevier BV

Subject

Condensed Matter Physics,Atomic and Molecular Physics, and Optics,Electronic, Optical and Magnetic Materials

Reference30 articles.

1. Radiation from rocket-exhaust plumes;Zirkind;Symp. (Int.) Combust.,1967

2. Infrared radiation signature of exhaust plume from solid propellants with different energy characteristics;Wang;Chin. J. Aeronaut.,2013

3. Handbook of infrared radiation from combustion gases (NASA;Ludwig;Washington,1973

4. Rocket exhaust plume phenomenology;Simmons,2000

5. IR radiation characteristics of rocket exhaust plumes under varying motor operating conditions;Niu;Chin. J. Aeronaut.,2017

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