[1]1 Stephens W D,Schwam W W,KruseR B,et a1.Application
of Fourier Transform Spectroscopy to Propellant Service
Life Prediction[R].AIAA76748,1976.
[2]Robert Feigley,Feng Jin,Jose Lorenzo,et a1.Monitoring
of Chemical Degradation in Propellants Using AOTF
Spectrometer[C].Proceedings of SPIE 5268,2004,96—1 03.
[3]Sammour M H.Stabilizer Reactions in cast Double Base
Rocket Propellant Part VI:Reactions of Propellant Stabilizers
with the Known Propellant Decomposition Products
N02,HN02 and HNO[J].Propellants,Explosives,Pyotechnics,
1995,20(3):126—134.
[4]Pettersson M.Stability Study of Smokeless Propellants of
up to 60 Years of Age as Measured by Heat Flow Calorimet-try[C].37thIntemational Annual Conference of ICT'Karl—
sruhe,Germany,June,2006.
[5]5 Little R R,Chelner H,Buswell H J.Development,Testing
and Application of Embedded Sensors for Solid Rocket
Motor Health Monitoring[C].37th International Annum
Conference of ICT,Kaflsruhe,Germany,June,2006.
[6]Cunliffe A V.Fraction Measurements-A Tool to Study
Cwss—Linking and Ageing in Composite Propellants and
PBXs[C].37th International Annual Conference of ICT,
Karlsrnhe,Germany,June,2006.
[7]Neviere R,Guyader M.DMA:A Powerful Technique to
Assess Ageing of MED[C].37th International Annual
Conference of ICT.Karlsrnhe,Germany,June,2006.
[8]Gottlieb L Migration of Plasticizer between Bonded Propellant
Interfac[J].Propellants,Explosives,Pyrotechnics,
2003,28(1):12-17.
[9]Grythe K F,Hansen F K.Diffusion Rates and the Role of
Diffusion in Solid Propellant Rocket Motor Adhesion[J].
Journal of Applied Polymer Science,2007,103(3):1529-
1538.
[lO]Freitas de Morals A M,Ribeiro Pinto J,Aguiar,J.Opti—
mization of Bondline Properties of Solid Rocket Motors
[C].37th International Annual Conference of ICT.Karlsruhe
。Germany,June,2006.
[1 1]HO S Y.Viscoelastic Response of Solid Rocket Motor
Components for Service Life Assessment[J].Journal of
Materials Science,1997。32(19):5155—5161.