Protection of ablative adhesion and erosion of slide track of missile launcher by high-temperature two-phase exhaust using MoS2-based bonded solid lubricant film

Mocaxue Xuebao/Tribology

Volumn 23, Issue 5, 2003, Pages 435-440

  Xiao, Jun ^a   Zhou, Hui Di ^b   Li, Tie Hu ^a   Zhang, Qiu Yu ^a   Chen, Jian Min ^b  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b LANZHOU INSTITUTE OF CHEMICAL PHYSICS   (China)

Author keywords

Ablation corrosion; Lubrication and protection; MoS2 bonded solid lubricant film; Rocket motor exhaust; Slide track

Indexed keywords

ABLATION; EROSION; MISSILE LAUNCHING SYSTEMS; MOLYBDENUM COMPOUNDS; PROTECTION; SOLIDS;

HIGH TEMPERATURE; MOLYBDENUM DISULFIDE; ROCKET MOTOR EXHAUST; SLIDE TRACK;

LUBRICANTS;

EID: 1942477320     PISSN: 10040595     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (7)

1. Xiao Jun, Shi Baoren, Guo Xiangsheng. Applied study on anti-corrosion of missile launcher at coastal area [J]. Marine Equipment, 1998, (9): 38-41.
2. Zhou Huidi, Hu Litian, Chen Jianmin, et al. Preparation and Tribological Behavior of a Bonded Solid Lubricating Coating for Application at High Specific Pressure [J]. Tribology, 2001, 21(5): 393-395.
3. Slikkerveer P J, it'tVeldF H. Model for patterned erosion [J]. Wear, 1999, 233-235: 377-386.
4. Lindsley B A, Marder A R. The effect of velocity on the solid particle erosion rate of alloys [J]. Wear, 1999, 225-229: 510-560.