Printed electronics are expanding as a commercial industry and have great potential
to advance space mission architecture. An end-to-end printed spacecraft has been
proposed by a team at the NASA Jet Propulsion Laboratory, and a potential area
that would greatly benefit from printed spacecraft are network missions. A proposed
mission concept is to release a large number of these printed spacecraft on Mars and
have them passively land to do basic sensing. In this work, we examine potential
passive surface landers to fulfill this goal.
The research presented here includes a survey of passive lander designs and an indepth analysis of an autorotator, a hexagonal pyramid, and a glider. Prototypes were designed, constructed, and tested experimentally for dispersion and
ight stability.
Monte Carlo simulations were developed for these vehicles in the Mars environment,
allowing an estimate of dispersion. Finally, a basic subsystem layout was developed
and some aspects of the communications and power subsystems for the spacecraft
were addressed.
Ultimately, the hexagonal pyramid and glider are recommended as potential surface
lander designs. The hexagonal pyramid design had excellent stability and packing
efficiency. However, the dispersion was estimated to only be on the order of tens of
thousands of square meters. The glider design had a predicted dispersion on the
order of tens of square kilometers, but suffered from potential stability issues in the
Mars environment. While the ideal platform depends on specific mission requirements,
through this work we develop insights and tools to characterize surface lander
performance that can be used in more advanced planning stages