The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.
SBC: BARBER-NICHOLS INC. Topic: T802
A rocket engine turbopump design using a partial emission pump combined with a zero net positive suction pressure inducer design is proposed to achieve a robust, deep throttling capability in 5k to 15k lbf thrust range rocket engines. A partial emission pump can provide better low-flow/thrust stability at a better efficiency than full emission pumps in this throttle range. A zero net positive suc ...STTR Phase I 2008 National Aeronautics and Space Administration
Integrating Prognostics in Automated Contingency Management Strategies for Advanced Aircraft ControlsSBC: Impact Technologies Topic: T101
Impact Technologies, in collaboration with Georgia Institute of Technology, proposes to develop and demonstrate innovative technologies to integrate prognostics into Automated Contingency Management (ACM) for advanced aircraft controls. Without consideration of prognostic information, the traditional reactive fault tolerant control approaches may fail to provide optimal fault mitigation/accommodat ...STTR Phase I 2008 National Aeronautics and Space Administration