Phase II Final Report - NASA's Institute for Advanced Concepts
Phase II Final Report - NASA's Institute for Advanced Concepts
Phase II Final Report - NASA's Institute for Advanced Concepts
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Chapter 3.0 Vehicle Design<br />
3.5 Fuel Storage and Production<br />
Based on the density of Inconel-718X (worst case), the RCM actuator with its internal components,<br />
plus the reaction chamber and fuel tank is estimated to weigh 0.3 kg. From Table 3-2, a<br />
reasonable fuel consumption rate is shown to be 0.011 kg/min. A ten minute flight with a 10%<br />
fuel reserve would thus require 0.12 kg of fuel, or 120 ml if the fuel were Hydrazine. This would<br />
there<strong>for</strong>e occupy 120 cm3 of fuel tank volume (about one quarter that of a cola can).<br />
The weight of the RCM system plus a 10 minute fuel charge is on the order of 0.42 kg. Based on<br />
Table 3-2, this would leave 1.08 kg <strong>for</strong> mission payload equipment.<br />
The design space identified by Table 3-2 is not believed to be optimum, but instead is only an<br />
example of one combination of flapping frequency, <strong>for</strong>ward speed, fuel type, etc. A parametric<br />
study to identify the boundaries of the design space is required be<strong>for</strong>e any determination of optimum<br />
per<strong>for</strong>mance can be assessed. Table 3-2 serves to show that Mars Entomopter operation is<br />
indeed possible with useful endurance and payload capacity. Nonetheless, it is still imperative<br />
that as much weight as possible be removed from the Entomopter frame of reference and placed<br />
on the refueling rover without loss of functionality.<br />
3.5 Fuel Storage and Production<br />
3.5.1 Introduction<br />
A number of mission scenarios have been proposed as a means to establish how to best utilize<br />
the capabilities of the Entomopter. From the evaluation of these missions, it became obvious that<br />
to maximize the potential of the Entomopter, it would need to be used in conjunction with either<br />
a lander or rover vehicle that would act as its base <strong>for</strong> communications, data and sample storage,<br />
and refueling. The ability to refuel the Entomopter is a critical element of the overall capability<br />
of the Entomopter and in providing a viable mission architecture. Without this capability the<br />
Entomopter would provide very little science return, because it would not be capable of flight<br />
<strong>for</strong> an extended period of time. There are two main approaches that can be taken to provide fuel<br />
<strong>for</strong> the Entomopter during its mission. The fuel can be carried from Earth and stored on the base<br />
vehicle or hydrogen can be brought from Earth, stored on the vehicle, and combined with elements<br />
gathered from the environment to produce fuel. Ideally, it would be possible to collect all<br />
the materials necessary to produce fuel on Mars from the soil or atmosphere. This would enable<br />
us to essentially have an infinite mission duration limited only by mechanical failure. However,<br />
based on the fuel and environmental survey, all practical fuels that can be used by the Entomopter<br />
require hydrogen (which is not available on Mars). There<strong>for</strong>e, the fuel chosen to be produced<br />
on the surface is hydrogen peroxide, which is simple to make and can be constructed out<br />
of the atmospheric gases with the addition of hydrogen.<br />
Because either producing the fuel on the surface or transporting it from Earth requires a finite<br />
supply of material from Earth (fuel or hydrogen), the determination of which method to utilize<br />
will be based on which one provides the longest mission duration <strong>for</strong> a given amount of weight.<br />
This is a critical determination because it will greatly affect vehicle propulsion system development<br />
by dictating the type of fuel that can be utilized. If it is determined that carrying hydrogen<br />
is more beneficial than a simple fuel such as hydrogen peroxide will be used. If it is determined<br />
that carrying the fuel from Earth is more beneficial, then a more complex energetic fuel can be<br />
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