Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Spacecraft and Rockets US/1993/5/

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21st century space transportation system design approach - HL-20 personnel launch system.pdf 2291KB Mar 28 2010 10:20:32 AM

Aerodynamic characteristics of the HL-20.pdf 854KB Mar 28 2010 10:20:32 AM

Aerodynamic heating environment definition thermal protection systemselection for the HL-20.pdf 1645KB Mar 28 2010 10:20:32 AM

Ascent abort capability for the HL-20.pdf 760KB Mar 28 2010 10:20:32 AM

Design for effective development and prototyping of the HL-20.pdf 1461KB Mar 28 2010 10:20:32 AM

Effect of lift-to-drag ratio in pilot rating of the HL-20 landing task.pdf 891KB Mar 28 2010 10:20:32 AM

Evaluation of the national launch system as a booster for the HL-20.pdf 852KB Mar 28 2010 10:20:32 AM

Experimental study of tail-span effects on a canard-controlled missile.pdf 581KB Mar 28 2010 10:20:32 AM

HL-20 computational fluid dynamics analysis.pdf 3374KB Mar 28 2010 10:20:32 AM

HL-20 concept - Design rationale and approach.pdf 1807KB Mar 28 2010 10:20:32 AM

HL-20 operations and support requirements for the Personnel Launch System mission.pdf 1472KB Mar 28 2010 10:20:32 AM

HL-20 subsystem design.pdf 1212KB Mar 28 2010 10:20:32 AM

Human factors evaluation of the HL-20 full-scale model.pdf 2404KB Mar 28 2010 10:20:32 AM

Preliminary structural evaluation and design of the HL-20.pdf 3468KB Mar 28 2010 10:20:32 AM

Six-degree-of-freedom guidance and control-entry analysis of the HL-20.pdf 713KB Mar 28 2010 10:20:32 AM

Titan III feasibility for HL-20 prototype missions.pdf 1086KB Mar 28 2010 10:20:32 AM