| NOW IT CAN BE TOLD ... |
_________________________________________________________ R E J E C T I O N O F O U R S U B M I T T A L . . . _________________________________________________________
| The following is the exact text of NASA's response to our SBIR Grant Proposal, as received on September 11, 2001, except that the text construct '[-UNDISCLOSED-]' has been used to replace certain proprietary technical details where they were mentioned. The term 'PI' means 'Principal Investigator', i.e. Larry Cottrill: |
Company Name: Cottrill Cyclodyne Corporation
Proposal #: SBIR 2001-I A8.02-9234
Project Title: Powerplant Which Transitions Automatically
to Ramjet Operation
Principal Investigator: Larry Cottrill
=Factor 1: Scientific/Technical Merit and Feasibility=
Reviewer 1 :
The proposal's idea of developing a viably efficient automatically
transitioning power plant to ramjet operation will undoubtedly have
ample commercial applications and will result in reduced costs compared
to present power plant designs. However, this proposal's scientific and
technical merits are not stated and explained clearly. Utilizing
ejector action to draw air into a power plant is a good idea but is not
clearly quantified and analyzed in this proposal. Flow patterns and
direction are not backed by scientific and detailed analysis and may not
be as PI describes in his narrative proposal. Reasoning and explanation
for flow patterns into [-UNDISCLOSED-] regions, and the [-UNDISCLOSED-]
region are not very rigorous and lack computational support and
validation. It is technically questionable whether such flow patterns
and mass flow rates can be achieved and are feasible with current design.
Reviewer 2 :
The concept presented contains inherent technical problems which
would limit the device to the point where this system would be
impractical for the application proposed. An explanation of the way in
which this concept would allegedly operate was presented, however, this
was not backed up with the necessary (even preliminary) analysis to
verify the performance claims are possible. The use of hydrogen fuel
was listed in the task descriptions, but no discussion of candidate
fuels and the selection of fuels was provided.
=Factor 2: Experience, Qualifications, and Facilities=
Reviewer 1 :
PI has a very diverse and wealthy background in a number of areas
applicable to parts of this effort, he has shown an ability to be a self
learner and perform well at what he does. However, PI lacks training in
the area of propulsion, especially in fluid dynamics and combustion.
To develop an efficient engine requires detailed knowledge in a number
of fields that PI does not posses. Facilities available for testing are
inadequate and they lack proper instrumentation and safety precautions.
Specially, in the area of understanding the flow behavior into the inlet
and [-UNDISCLOSED-] and combustion process which are crucial for PI's
power plant success.
Reviewer 2 :
The principal investigator has no vocational experience in
propulsion system design. He has a fairly broad background in several
supporting disciplines which would help him carry out this proposed
activity. His formal education is significantly limited (no college
degree, some virtually un-related college course work). He currently is
the sole employee of this company and, therefore, does not currently
have any individuals with strong relevant background, training, or
experience immediately available to assist in this proposed activity.
No analytical results were presented to provide a technical foundation
for the concept, and to demonstrate the technical knowledge of the
principal investigator.
=Factor 3: Effectiveness of the Proposed Work Plan=
Reviewer 1 :
PI has a detailed comprehensive work plan. PI seems to have a very
good handle on design and fabrication issues and timetables related to
that. PI has performed pricing of the essential items required for
completion of listed tasks and optimizes use of resources he is
requesting.
Reviewer 2 :
The proposed work has a strong experimental element which will
directly examine the operation of this device. There was not any
significant analytical/ computational effort described which would be
necessary to interpret the performance results observed. The scope
of the test (due to the relatively simple design of the design) would
probably be do-able by the principal investigator and subcontractor.
Safety issues surrounding this experimental activity (particularly the
use of hydrogen fuel) were not addressed.
=Overall Technical Evaluation=
Reviewer 1 :
Reviewer 2 :
The primary strength is the principal investigator appears to be an
innovative individual and is motivated to explore his idea and will work
hard in an attempt to make this device operate. A strength is also the
relatively simple design and construction of this device. A weakness is
the limited background and experience of the principle investigator in
this technical area. A weakness is the inherent technical challenges of
this device as shown which would make it impractical for the system
proposed. No specific analysis was presented which would show the device
could be made to operate in the manner described.
=Factor 4: Commercial Merit and Feasibility=
Reviewer 1 :
Reviewer 2 :
With some re-design and development an "engine" with some of the
features included in this device may be useful in the scale model
market.
=Comments on NASA Facility Requirements=
[note: No NASA facilities were requested]
Reviewer 1 :
Reviewer 2 :
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| Larry Cottrill discussing design of the recycled-exhaust driven
ejector intake [NOTE: No proprietary or patentable design elements are illustrated in this photo]
Photo Copyright 2003 Cottrill Cyclodyne Corporation |
The CYCLODYNETM general aviation powerplant
- now under development by