RHRC & CAL POLY SAN LUIS OBISPO AWARDED NASA SMALL BUSINESS
October 23, 2009 - Rolling Hills Research Corporation
and California Polytechnic State University San Luis Obispo have been selected by NASA for a $600,000
Phase II Small Business Technology Transfer (STTR) research contract. The
funding for this program was made possible by the American Recovery and
Reinvestment Act (ARRA) of 2009.
The proposed innovation is to use the refrigerant
capabilities of nitrous oxide (N2O) to provide the cooling required
for reusable operation of an aerospike nozzle in conjunction with an N2O-HTPB
(hydroxyl-terminated polybutadiene, a synthetic rubber that is used as a binder
in solid rocket motors and as a fuel in hybrid rocket motors) hybrid rocket
motor. The phase change cooling as liquid N2O is flashed into a vapor
is crucial to limiting to acceptable levels the erosion of both the nozzle
throat and spike, thereby enabling reusable operation and/or long burn times.
The N2O used for cooling the nozzle throat will be reintroduced into
the combustion chamber, and the N2O used for cooling the spike will
be used to provide base bleed, virtually eliminating any performance penalty
associated with using a severely truncated, and therefore significantly lighter,
spike. Because of its high vapor pressure, N2O can be self-pumping,
thereby making it an ideal choice of oxidizer for simple, low-cost applications.
As a simple, practical nozzle, the proposed innovation fits well with N2O-HTPB
hybrid rocket designs, which tend toward simpler, less expensive design
alternatives. Because of their high efficiency due to altitude compensation,
aerospike nozzles could play an important role in bringing to fruition
inexpensive access to low Earth orbit. The simple, low-cost, reusable,
oxidizer-cooled aerospike nozzle for operation on an N2O-HTPB hybrid
rocket motor that is proposed will enable much-needed flight research of
aerospike nozzles. These oxidizer-cooled altitude-compensating nozzles promise
significant improvements in propulsion efficiency for a wide range of space
vehicles and tactical missiles.
For this project, RHRC will provide overall program
management, while CPSU will provide technical leadership. RHRC will also
perform the complex CFD analysis required to predict the atomization and
phase-change cooling provided by the N2O. CPSU will perform
validation experiments with hot gas flow on their rocket test bench.
Dr. Bill Murray of CPSU will be the Principal Investigator
and lead his team of: Dr.
Patrick Lemieux, Dr. Joseph
Mello, Mr. Jim Gerhardt,
and Mr. Terry Cooke.
Dr. Mike Kerho of RHRC will perform the CFD
analysis for this research program.