A dozen inventors have received a chance to demonstrate the potential
for their pet space projects as winners of NASA's 2013 Innovative
Advanced Concepts (NIAC) Program Phase I awards. The winners were chosen
based on their potential to transform future aerospace missions by
enabling either breakthroughs in aerospace capabilities or entirely new
missions. Read on for a closer look at some of the most promising
proposals with a view to how they would work, and where the tricky bits
might be hiding.
Each NIAC Phase I winner receives about US$100,000 to spend a year
pursuing their ideas, including an initial feasibility study of a novel
aerospace concept. The proposals this year include; 3D printing of
biomaterials; using galactic rays to map the insides of asteroids; and
an "eternal flight" platform that could hover in the Earth's atmosphere.
The list of this year's awardees includes:
- Rob Adams of NASA Marshall Space Flight Center – Pulsed Fission-Fusion (PuFF) propulsion system
- John Bradford of SpaceWorks Engineering – Torpor inducing transfer habitat for human stasis to Mars
- Hamid Hemmati of NASA Jet Propulsion – Two-dimensional planetary surface landers
- Nathan Jerred of Universities Space Research Association - Dual-mode
propulsion system enabling CubeSat exploration of the Solar System
- Anthony Longman – Growth adapted tensegrity structures
- Mark Moore of NASA Langley Research Center - Eternal flight as the solution for 'X'
- Thomas Prettyman of the Planetary Science Institute – Deep mapping
of small solar system bodies with galactic cosmic ray secondary particle
showers
- Lynn Rothschild of NASA Ames Research Center – Biomaterials out of thin air
- Joshua Rovey of the University of Missouri – Plasmonic force propulsion revolutionizes Nano/PicoSatellite capability
- Adrian Stoica of NASA Jet Propulsion Lab – Transformers for extreme environments
- Christopher Walker of the University of Arizona – 10 meter sub-orbital balloon refletor
- S.J. Ben Yoo of the University of California-Davis – Low-mass planar photonic imaging sensor
Let's take a look at three of the most promising concepts with a view
to how they would work, and where the tricky bits might be hiding.
Rob Adams' PuFF pulsed fission-fusion propulsion system
The PuFF propulsion system is a new take on an old idea. To confine a
deuterium-tritium plasma to act as a breakeven reactor. People have
been trying this seriously for half a century and have not yet
succeeded. To base a space drive on such a thing would be extremely
speculative.
In the PuFF approach, however, the fusion of the deuterium-tritium
fuel is only the first stage of the process. Instead of seeking a
particular power output, the fusion reaction is being carried out to
provide a source of neutrons. This D-T reaction releases a 3.5 MeV alpha
particle, and a neutron with 14.1 MeV of kinetic energy.
As seen above, in a second stage of nuclear reaction the fusion
neutrons can be captured by a uranium nucleus, thereby causing it to
fission, releasing some 200 MeV of nuclear energy. Because of the high
energy of the fusion neutrons, four to five neutrons will generally be
released from uranium fission, rather than the two to three seen with
thermal neutrons.
If you send a neutron into a critical mass of fissile material, the
resulting chain reaction continues until the critical mass explodes.
However, if you have a bit less than a critical mass, the total number
of fissions resulting from the input of a swarm of fission neutrons is
rather impressive.
Impact of 1,000 fusion neutrons on uranium nuclei will initially
cause 1,000 uranium atoms to fission. This will release about 5,000
neutrons in the uranium, owing to the large energy of the fusion
neutrons. If the fissile material is one percent away from being a
critical mass, some of these neutrons will escape the uranium, but
enough will cause fissions that produce 0.99 times 5,000, or 4,950
neutrons. This requires about 1,980 fissions. In the next step, the
4,950 neutrons cause fissions that produce 0.99 times 4,950 neutrons, or
4,900 neutrons, which requires 1,960 fissions.
As the chain goes on, it eventually runs out of steam, as shown by
the reduction in the number of neutrons. However, in the course of the
not quite critical chain reaction, roughly 200,000 uranium nuclei will
have undergone fission. Uranium fission releases about 200 MeV of
energy. The original 1,000 fusions that produce the 1,000 free neutrons
releases about 19 GeV, but the resulting fissions release about 40,000
GeV. Coupling the fusion neutrons into a not quite critical mass of
uranium results in an amplification of the fusion power by a factor of
about 2,100, providing plenty of power for a spacecraft drive!
A pulsed drive based on the fusion-fission combination process need
not achieve fusion breakeven. Instead, the focus is on fusion-based
neutron generation followed by fission-based neutron multiplication. The
very largest inertial confinement machines at present produce tens of
megajoules per pulse. If the neutron output were directed into a
PuFF-type fusion-fission drive, the total nuclear output per pulse could
easily be 10 GJ, or about 3 MWh energy release each second – probably
1,000 times the power needed to power a spaceship drive, leaving plenty
of room for engineering compromise.
Nathan Jerred's Small-scale Dual-mode Propulsion System
A considerable number of exploratory designs have surfaced, with the
common intent of using the nano/pico satellite/probe concept past
low-earth orbit. Most of these are single-principle drives, which would
be found lacking under some circumstances. For example, a
CubeSat
might be able to reach velocities required for interplanetary travel
using a solar powered ion drive. However, a large number of trajectories
would not be feasible because the ion drive does not provide enough
thrust for course alteration, course correction, orbital insertion, or
other astronavigation challenges.
In such nanoprobes it seems unlikely that two independent propulsion
systems can be shoehorned into place while still having adequate
performance for interplanetary missions. Jerred's dual-mode propulsion
system is a new attempt to address this problem.
The two modes of which he speaks are a thermal drive and an ion
drive. The source of power for both would be radioactive decay, probably
of a mass of plutonium 238 (Pu-238). Such radioactive sources have been
used in many space missions to provide a heat source for a radioisotope
thermoelectric generator (RTG). An RTG powers the
Cassini mission, the
Mars rover Curiosity, and the New Horizons mission to Pluto.
In Jerred's dual-mode drive, a modified RTG provides power for both
drive modes. For the thermal drive, reaction mass in the thermal
propulsion propellant tanks is fed through the RTG, therein being heated
to about 850° C (1,500° F). This is more than enough to gassify the
propellant and generate a high pressure, after which it expands through
the nozzle to produce thrust.
Without more engineering information it is very difficult to evaluate
how much thrust, but it should be on the order of one Newton (about 1/4
lb). The specific impulse should be in the neighborhood of 300 sec,
similar to that of chemical fuels. Running the RTG at a higher
temperature is a possibility, which would result in larger specific
impulse, but higher temperatures put a strain on the Stirling RTG
components.
The second mode of propulsion is the ion drive. In this case, the RTG
operates to produce electricity for an ion drive. An RTG that provides 1
kW of heat and about 300 W of electrical power would require about 2 kg
(4.4 lb) of Pu-238, the most common isotope used in RTGs. But Pu-238
has a half-life of almost 90 years, which is overkill for, say, a
mission to an asteroid or to Mars. If two to three months of propulsive
power would be enough for a mission, polonium 210 could be used. It has a
half-life of 138 days, and only about 15 g (0.5 oz) would be required
to produce 1 kW of heat.
The sample mission for the proposed study is to send a 10 kg (22 lb)
payload to Europa. The Phase I study will provide engineering analysis
of the major components and look at performance-related compromises
which will help determine the feasibility of such a mission. Positive
results may lead to an 18 month study that examines the sample mission
in more depth.
John Bradford's Torpor to Mars Missions
One problem with space flight at our current state of advancement is
that it takes too long. Flight times within the solar system are
measured in months or years, during which time astronauts would
generally have very little to do, but continue to consume full helpings
of food, water, oxygen, and power. Psychologists also suggest that the
interminable boredom of long-duration space flights may present
substantial difficulties for a crew.
Science fiction has often resorted to inducing suspended animation to
avoid these dull periods. The problem with looking to suspended
animation for a solution is that humans seem to lack the ability to
safely achieve significant levels of hibernation or torpor. Despite
this, the profound medical applications that reduced metabolism states
could offer have stimulated considerable research on just what causes
hibernation, how it differs from torpor, and how it might be induced in
mammals without natural access to these states. John Bradford has
convinced NASA that it is time to take a serious look for applications
in space travel.
The idea isn't to freeze people and thaw/resuscitate people at Mars,
or to induce hibernation. True hibernation occurs when an animal allows
it's heart rate to drop precipitously, and its body temperature to drop
to a few degrees above ambient.
A better model is likely to be a wintering bear. Bears do slow their
heart rate to as low as 10 beats per minute (it's normally about 40 when
asleep), but only drop their body temperature by about 5° C (9° F).
Their long winter sleep is more often called torpor, or winter lethargy.
This is the general pattern among the larger mammals which "hibernate."
By analogy, people are expected to enter more easily into extended
torpor than into true hibernation.
Considerable experimentation has been done in search of triggers for
torpor. In the area of drug-like triggers, one study showed rather
conclusively that small quantities of hydrogen sulfide in the air would
induce a hibernation-like state. Their body temperature fell to about 2°
C (4° F) above ambient, and their breathing rate fell by more than 90
percent. Their blood pressure, however, remained high. Researchers have
also been able to induce torpor in pigs for several hours without
apparent damage.
John Bradford is taking what is known about torpor to perform a
"what-if" study. His project will design a torpor module for astronauts
on a slow boat to Mars, and will compare the supply and mission
requirements for a range of conventional technology assumptions for such
missions. This Phase I analysis is only intended to investigate the
compatibility of a torpor module with inner solar system voyages. Later
in the program, if renewed, he will study how to accomplish the goal of
induction and maintenance of torpor in a crew of astronauts.