Loading…
Experimental lifetime study of regeneratively cooled rocket chamber walls
•Provocation of the ’doghouse’ failure mode under well-defined conditions.•Effects of various load conditions on the lifetime of thrust chamber walls.•Progression of deformations and surface roughness of thrust chamber walls.•Effects and behavior of thermal barrier coatings under hot-gas conditions....
Saved in:
Published in: | International journal of fatigue 2020-09, Vol.138, p.105649-12, Article 105649 |
---|---|
Main Authors: | , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Summary: | •Provocation of the ’doghouse’ failure mode under well-defined conditions.•Effects of various load conditions on the lifetime of thrust chamber walls.•Progression of deformations and surface roughness of thrust chamber walls.•Effects and behavior of thermal barrier coatings under hot-gas conditions.•Discussion of lifetime limiting mechanisms in rocket combustion chambers.
A detailed knowledge of the life-limiting mechanisms of regeneratively cooled rocket combustion chambers is important to increase the safety, the thrust-to-weight ratio and the cost-efficiency of future rocket engines. For this purpose, an actively cooled specimen made of CuCr1Zr is mounted downstream of a combustion chamber. The specimen is loaded cyclically and inspected after each cycle. The specimens collapse in the ’doghouse’ failure mode after several load cycles. The effects of different hot-gas and coolant conditions, surface roughness and thermal barrier coatings on the lifetime are studied. The life-limiting mechanisms: creeping, yielding, abrasion, blanching and thermal aging are discussed. |
---|---|
ISSN: | 0142-1123 1879-3452 |
DOI: | 10.1016/j.ijfatigue.2020.105649 |