Comprehensive analysis and estimation system on thermal environment, heat protection and thermal structure of spacecraft

Acta Astronautica

Volumn 54, Issue 5, 2004, Pages 347-356

  Guoliang, Mao ^a   Guiqing, Jiang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; AERODYNAMIC HEATING; AEROSPACE ENGINEERING; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DATA REDUCTION; DATABASE SYSTEMS; EXPERT SYSTEMS; HEAT FLUX; HEAT PROBLEMS; HEAT SHIELDING; MATHEMATICAL MODELS; PRESSURE DISTRIBUTION; REENTRY; TEMPERATURE DISTRIBUTION; THERMAL STRESS;

ABLATION PROTECTION; HEAT PROTECTION;

SPACECRAFT;

EID: 0346963779     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(03)00035-3     Document Type: Article

References (4)

1. G.Q. Jiang, et al., Comprehensive Analysis and Estimation System of Thermal Environment, Heat Protection and thermal Structure of Spacecraft, Beijing Institute of Aerodynamics, Beijing, 1999, p. 4 (in Chinese).
2. Q. Chen, An Extenuated Object Oriented Date Basic Approach, 10th International Computer Software and Applications Conference, 1987.
3. F. Mancle, J. Orenstcin, Toward a general spatial data model for an object-oriented, DBMS, Para of VLDB D, 1985.
4. E.A. Rich, Artificial Intelligence, New York, 1983.