A new class of material is now being developed
for cryogenic thermal insulation systems for the next-generation reusable
launch vehicles, commercial and defense marine ships, commercial aircraft,
and numerous industrial applications. Recent advancements in high-temperature
polymeric materials at the NASA Langley Research Center have led to the
development of new polyimide foam systems with attractive properties for
applications in thermal and acoustic insulation. To understand the performance
parameters of these new foam systems at low temperatures and pressures,
experimental studies are being conducted at the Cryogenics Test Laboratory.
Liquid nitrogen cryostats developed by the Cryogenics Test Laboratory are
being used to perform detailed thermal characterizations of these novel
materials under full-range cryogenic vacuum conditions. Although common
polymeric foams such as polyurethane have outstanding properties, they
have been limited in their applications by temperature, poor fire resistance,
and their susceptibility to thermal cycling and ultraviolet light exposure.
These new high-performance foam systems of cyclic imide polymers have excellent
structural integrity, fire resistance, thermal aging resistance, and thermal
cycling properties.
In general, thermal conductivity of foamed systems is the lowest
of any solid materials and is determined by the gaseous conduction
within the
pores, conduction via the solid structure of the foam, convection through
the cells, and radiative heat transfer. This research allows for all
of these parameters to be studied, including density, surface
area, and open-
or closed-cell content effects. In closed-cell foams, the heat transfer
coefficient in the cell will change as the blowing agent is replaced
by air with time. In open-cell foams, the overall thermal conductivity
of
the system will increase because of the open transfer of air into the
cells through convection. This pioneering work involves never-before-investigated
parameters for these foam systems and has led to important technology
development
for the NASA Space Launch Initiative/2nd Generation Launch Vehicles
Program. The research and development are now being extended
for the future utilization
of novel polyimide composite materials in both aerospace launch systems
and a number of industrial cryogenic equipment applications. |
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Insulation Test Articles of Polyimide Foam Materials
Key accomplishments:
- Pioneering work
involved never-before-studied thermal conductivity parameters for
polyimide foams and composite systems.
- A total of 104
cryogenic tests of 12 different materials was performed in 2001.
- A new flat-plate
cryogenic insulation test apparatus was constructed.
- Baseline research
led to important work for the Space Launch Initiative/2nd Generation
Launch Vehicles Program
- Research led
to a Shuttle launch site equipment project proposal that addresses
replacement of cryogenic insulation for ground systems.
Key milestones:
- Cryogenic performance
information of polyimide foams was provided to support Phase I technology
development work for the Space Launch Initiative.
- A number of publications
and presentations on related polyimide foam research, including an
American Chemical Society book chapter, were made in 2001.
Contacts: M.K. Williams (Martha.Williams-1@ksc.nasa.gov),
YA-C2, (321) 867-4554; J.E. Fesmire, YA-C2, (321) 867-7557; and J.W.
Gay, YA-F2-T1, (321) 867-9195
Participating Organizations: NASA Langley Research Center (E. Weiser) and Dynacs
Inc. (Dr. S.D. Augustynowicz and K.W. Heckle, Sr.)
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