Orbital re-entry experiment vehicle ground and flight dynamic test results comparison

Journal of Spacecraft and Rockets

Volumn 33, Issue 5, 1996, Pages 635-642

  Yoshinaga, Takashi ^a,b,c   Tate, Atsushi ^a,b   Watanabe, Mitsunori ^a,b   Shimoda, Takayuki ^a,d  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Supersonic Wind Tunnel Contr Sect

^c Supersonic Wind Tunnel Contr Sect ^*

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; APPROXIMATION THEORY; CALCULATIONS; MATHEMATICAL MODELS; ORBITS; TRANSONIC AERODYNAMICS; WIND TUNNELS;

ANGULAR MOTION; ORBITAL RE ENTRY EXPERIMENT; SINGLE DEGREE OF FREEDOM TEST METHOD;

REENTRY;

EID: 0030230299     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/3.26813     Document Type: Article

References (12)

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11. Yoshinaga, T., Tate, A., and Inoue, K., "Phase Plane Analysis for Non-Linear Oscillation of Bodies at High Angles of Attack," IUTAM Symposium of Fluid Dynamics of High Angle of Attack, edited by R. Kawamura and Y. Aihara, Springer-Verlag, Berlin, 1992, pp. 301-310.
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