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Company Information:

Company Name:
TechLand Research, Inc.
Address:
28895 Lorain Road
Suite 201
North Olmsted, OH
Phone:
(440) 716-9077
URL:
N/A
EIN:
311565119
DUNS:
967185414
Number of Employees:
5
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $528,433.00 8
SBIR Phase II $1,836,690.00 3

Award List:

Design Of A High Performance External-Compression Inlet For Cruise At Mach 2.4

Award Year / Program / Phase:
1997 / SBIR / Phase I
Award Amount:
$69,902.00
Agency:
NASA
Principal Investigator:
Bobby W. Sanders , SENIOR SCIENTIST
Abstract:
N/a

Mixed-Compression Inlet for Supersonic Cruise with High Performance and Operability

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$69,948.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

Design Of A High Performance External-Compression Inlet For Cruise At Mach 2.4

Award Year / Program / Phase:
1998 / SBIR / Phase II
Award Amount:
$592,694.00
Agency:
NASA
Principal Investigator:
Bobby W. Sanders , SENIOR SCIENTIST
Abstract:
N/a

N/A

Award Year / Program / Phase:
2000 / SBIR / Phase I
Award Amount:
$69,918.00
Agency:
NASA
Principal Investigator:
Lois J. Weir, C.E.O.
Abstract:
N/a

Flight Testing of a New Design Concept for Axisymmetric Inlets

Award Year / Program / Phase:
2001 / SBIR / Phase II
Award Amount:
$599,974.00
Agency:
NASA
Principal Investigator:
Lois J. Weir, C.E.O.
Abstract:
This proposal identifies a flight test program on the F-15B at NASA Dryden to obtain off-design performance of high-speed inlets that incorporate a unique variable geometry system. The proposed effort accomplishes two objectives; validation of engine face distortion prediction by complex CFD codes… More

Flight Testing of a New Design Concept for Axisymmetric Inlets

Award Year / Program / Phase:
2001 / SBIR / Phase I
Award Amount:
$0.00
Agency:
NASA
Principal Investigator:
Lois J. Weir, C.E.O.
Abstract:
This proposal identifies a flight test program on the F-15B at NASA Dryden to obtain off-design performance of high-speed inlets that incorporate a unique variable geometry system. The proposed effort accomplishes two objectives; validation of engine face distortion prediction by complex CFD codes… More

High-Performance, Low-Sonic-Boom Supersonic Cruise Inlet

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$69,653.00
Agency:
NASA
Principal Investigator:
Bobby W. Sanders, Principal Investigator
Abstract:
This proposal describes a research study to define a high-speed inlet model for flight-testing on the F-15B at NASA Dryden. The objectives of the flight test program are to obtain off-design performance and shock wave signatures for a high-speed inlet designed for supersonic cruise. This proposal… More

Airflow Controller and Isolator for Pulse Detonation Engines

Award Year / Program / Phase:
2003 / SBIR / Phase II
Award Amount:
$644,022.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Bobby W. Sanders, President
Abstract:
The development of a revolutionary airflow controller and isolator for application with a high-speed inlet and a pulse detonation engine (PDE) is proposed. This innovation has the potential of providing a solution to the unique airflow-matching problemimposed by the integration of a PDE with a… More

Airflow Controller and Isolator for Pulse Detonation Engines

Award Year / Program / Phase:
2003 / SBIR / Phase I
Award Amount:
$99,129.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Bobby W. Sanders, President
Abstract:
A revolutionary airflow controller and isolator for application with a high-speed inlet and a pulse detonation engine (PDE) is proposed. This innovation has the potential of providing a solution to the unique airflow matching problem imposed by theintegration of a PDE with a high-speed inlet. The… More

Mode Transition Variable Geometry for High Speed Inlets for Hypersonic Aircraft

Award Year / Program / Phase:
2005 / SBIR / Phase I
Award Amount:
$69,915.00
Agency:
NASA
Principal Investigator:
Lois J. Weir, Principal Investigator
Abstract:
Hypersonic propulsion research has been a focus of the NASA aeronautics program for years. Previous high-speed cruise and space access programs have examined the problems of inlet design for hybrid systems, mainly by addressing one part of the flight envelope only. The proposed program will… More

Design of a Highly Compact Supersonic Cruise Missile (SSCM) Inlet

Award Year / Program / Phase:
2012 / SBIR / Phase I
Award Amount:
$79,968.00
Agency:
DOD
Principal Investigator:
Lois Weir, CEO – (440) 716-9077
Abstract:
The objective of the proposed effort is to demonstrate the feasibility of designing a Mach 2.5 inlet for a high-speed cruise missile. This inlet must provide the proper airflow to a turbojet engine for flight Mach numbers from 0.4 to 2.5. It must be light weight, be compact, have low cost and simple… More