International Journal of Engineering Research in Computer Science and Engineering (IJERCSE)

Review on Aerocapture

Author : Pramod Kumar ¹

Date of Publication :25th January 2017

Abstract: Aerocapture can be defined as an aircraft venturing out from Earth to another planet on a ballistic direction approaches that planet at hyperbolic speed. Generally, this deceleration has been accomplished by propulsive catch, which devours a lot of charge. Aerocapture offers a more eco-friendly option by exploiting vehicular drag in the planet's climate. This system creates extraordinary heat thatâ€™s why it requires a â€œspecial thermal protection shieldâ€. This paper objective is to investigate the outcome of an Aerocapture recreation device (ACAPS) created in MATLAB with SIMULINK, accentuating code approval, upgradeability, user friendliness and direction perception. The present variant of ACAPS 1.1 is having 3 dof and point mass reproduction model that fuses a look-into table for the Mars environment. ACAPS is required to enhance the National Aeronautics and Space Administration (NASA) Jet Propulsion Laboratory (JPL) Project Design Center (PDC) as fundamental plan programming for the Mars Sample Return (MSR), Mars Micro missions, Neptune/Triton Mission, and Human Mars Mission.

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