Effect of Spacecraft Aerodynamics and Heat Shield Characteristics on Optimal Aeroassisted Transfer

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ISSN Print: 1947-3931
ISSN Online: 1947-394X
www.scirp.org/journal/eng
E-mail: eng@scirp.org

"Effect of Spacecraft Aerodynamics and Heat Shield Characteristics on Optimal Aeroassisted Transfer"
written by Antonio Mazzaracchio, Mario Marchetti,
published by Engineering, Vol.4 No.6, 2012

has been cited by the following article(s):

[1]	Coupled versus uncoupled optimal solutions for thermal and dynamic problems in spacecraft atmospheric flight
	World Journal of Engineering, 2016

[2]	Flight-Path Angle Guidance for Aero-Gravity Assist Maneuvers on Hyperbolic Trajectories
	2016

[3]	Flight-Path Angle Guidance for Aerogravity-Assist Maneuvers on Hyperbolic Trajectories
	Journal of Guidance, Control, and Dynamics, 2014

[1]	Flight-Path Angle Guidance for Aero-Gravity Assist Maneuvers on Hyperbolic Trajectories AIAA Guidance, Navigation, and Control Conference, 2016 DOI:10.2514/6.2016-1371

[2]	Coupled versus uncoupled optimal solutions for thermal and dynamic problems in spacecraft atmospheric flight World Journal of Engineering, 2016 DOI:10.1108/WJE-02-2016-006

[3]	Flight-Path Angle Guidance for Aerogravity-Assist Maneuvers on Hyperbolic Trajectories Journal of Guidance, Control, and Dynamics, 2015 DOI:10.2514/1.G000670

[4]	Heat Shield Mass Minimization for an Aerocapture Mission to Neptune International Journal of Aerospace Innovations, 2013 DOI:10.1260/1757-2258.5.3-4.83

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