Probability of Solid-Propellant Motor Failure Due to Environmental Temperatures-Reference-Cited by-同舟云学术

Probability of Solid-Propellant Motor Failure Due to Environmental Temperatures

Published:1979-05 Issue:3 Volume:16 Page:140-146
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Heller R.A.¹,Kamat M.P.¹,Singh M.P.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57634

Reference14 articles.

1. Temperature response of an infinitely thick slab to random surface temperatures

2. 2Heller, R.A. "Thermal Stress as a Narrow-Band Random Load," American Society of Civil Engineers, EM5,No. 12450,Oct. 1976, pp.787-805; also, U.S. AMICOM. TR.RK-7T-1, May 7, 1976.

Cited by 28 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental Investigation on Fracture Properties of HTPB Propellant with Circumferentially Notched Cylinder Sample;Propellants, Explosives, Pyrotechnics;2022-05-27

2. Life Interval Prediction for Aging Solid-Propellant Rocket Motors with Uncertain Chemical Parameters;Journal of Spacecraft and Rockets;2021-10-06

3. Ageing studies on AP/HTPB based composites solid propellants;Energetic Materials Frontiers;2021-06

4. Accelerated ageing of composite solid propellants under cyclic temperature variations;Journal of Energetic Materials;2020-09-12

5. Effect of cyclic loads on structural damage of rocket propellant grain;Scientific Technical Review;2019