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A fundamental question for Astrobiology is the question of the ability of life to expand beyond its planet of origin. Introducing life on Mars is the likely near-term step in addressing this question. Making Mars more suitable for life (terraforming) involves altering the martian environment so that microorganisms and plants from Earth could survive there. We define two principal goals: 1) determine the minimal change in pressure, gas composition, and temperature on Mars that would allow for growth of plants from arctic and alpine biomes. 2) Determine the characteristics of plant growth at 0.38 g. This paper reviews martian environmental factors in the context of plant survival, and discusses the use of Space Station as a hypogravity testbed.

This paper summarizes the recent development of an adaptive aeroelastic wing shaping control technology called variable camber continuous trailing edge flap (VCCTEF). As wing flexibility increases, aeroelastic interactions with aerodynamic forces and moments become an increasingly important consideration in aircraft design and aerodynamic performance. Furthermore, aeroelastic interactions with flight dynamics can result in issues with vehicle stability and control. The initial VCCTEF concept was developed in 2010 by NASA under a NASA Innovation Fund study entitled “Elastically Shaped Future Air Vehicle Concept,” which showed that highly flexible wing aerodynamic surfaces can be elastically shaped in-flight by active control of wing twist and bending deflection in order to optimize the spanwise lift distribution for drag reduction. A collaboration between NASA and Boeing Research & Technology was subsequently funded by NASA from 2012 to 2014 to further develop the VCCTEF concept.