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SBC: M4 ENGINEERING, INC. Topic: MDA18T006
Uncertainty Reduction in High Speed Flight Vehicle Modeling | Approved for Public Release 18-MDA-9707 (3 Jul 18)STTR Phase I 2019 Department of DefenseMissile Defense Agency
Test Article Printing with Laser Additive Manufacturing (TAP-LAM) for Threat Surrogate Target ProductionSBC: MV Innovative Technologies LLC (DBA: Opt Topic: MDA17T001
Optonicus proposes development of the TAP-LAM (Test Article Printing with Laser Additive Manufacturing for Threat Surrogate Target Production) powder bed fusion and directed energy depositions systems. The TAP-LAM metal additive manufacturing system will advance strategic missile defense system testing capabilities by improving 3D printing methods to rapidly produce large-scale threat surrogate ta ...STTR Phase I 2018 Department of DefenseMissile Defense Agency
SBC: POLARIS SENSOR TECHNOLOGIES INC Topic: SOCOM18A001
The objective of this proposal is to develop instrumentation and algorithms for acquiring facial features for facial recognition in low- and no-light conditions.We will use cross-spectrum matching by exploiting infrared polarimetric imagery which tends to show features that match more closely visible imagery than conventional infrared.In addition to thermal infrared, we will also test subjects in ...STTR Phase I 2018 Department of DefenseSpecial Operations Command
SBC: PIONEER ASTRONAUTICS Topic: MDA18T005
he Storable Clean Ethane-ethylene Nitrous Engine (SCENE) is a proposed technology designed to provide upper stages and spacecraft with non-toxic, liquid, non-cryogenic, high-performance propulsion with an Isp on the order of 300 seconds. The propellant components are stored as liquids under their saturated vapor pressures. With the SCENE, nitrous oxide is used as an autogenously pressurized oxidiz ...STTR Phase I 2019 Department of DefenseMissile Defense Agency
SBC: DGNSS Solutions, LLC Topic: MDA09T003
The primary objective of the proposed research is to develop proof of concept of a software programmable X-Band radar system using low cost antenna array technology with digital beamforming architecture based on multiple receiver channels. The performance objectives will aim at a minimum of 400 MHz instantaneous bandwidth and a minimum instantaneous dynamic range of 52 dB. The objective of the t ...STTR Phase I 2010 Department of DefenseMissile Defense Agency
SBC: WECOSO, INC. Topic: MDA17T003
West Coast Solutions (WCS), in collaboration with the Georgia Institute of Technology and Creare LLC, proposes an adaptation of our SmallSat Stirling Cryocooler (SSC) technology in response to STTR Topic MDA17-T003: High-Efficiency, Low-Volume, Space-Qualified Cryogenic-Coolers. In Phase 1 we will scale up a design currently in development for NASA to meet the Missile Defense Agency (MDA) topic re ...STTR Phase I 2018 Department of DefenseMissile Defense Agency
SBC: IRIS TECHNOLOGY CORPORATION Topic: MDA17T003
The Iris Technology team which also include Northrop Grumman Aerospace Systems (NGAS) and the University of Wisconsin, is attacking the problem of high-efficiency, low-volume, space-qualified cryocooler systems.The team has a firm starting point by leveraging the Northrop Grumman Microcryocooler and the Iris Technology mLCCE (Miniature Low Cost Control Electronics).TMU enhancement will start with ...STTR Phase I 2018 Department of DefenseMissile Defense Agency
SBC: DECIBEL RESEARCH, INC. Topic: MDA12T002
The development and integration of three unique and innovative algorithm prototypes into a"Fused Track and Characterization Schema"are proposed. This Schema will encompass the determination of signatures and characteristics of objects that can be identified by RF and EO/IR Sensors in order to enable multi-sensor data fusion and correlation. The first algorithm, the"3D Pose Estimation"Algorithm, p ...STTR Phase I 2013 Department of DefenseMissile Defense Agency
SBC: METACOMP TECHNOLOGIES INC Topic: MDA09T009
The occurrence of combustion instability has long been a matter of serious concern in the development of liquid-propellant rocket engines due to the high rate of energy release in a confined volume in which energy losses are relatively small. Positive feedback between the acoustic waves and unsteady combustion could lead to the destruction of an engine in a fraction of a second. The situation is ...STTR Phase I 2010 Department of DefenseMissile Defense Agency
SBC: ATMOSPHERIC & SPACE TECHNOLOGY RESEARCH ASSOCIATES LLC Topic: MDA16T005
Future, large footprint weapon systems can benefit from a multi-frequency telemetry system that provides support for multiple bands and various Advanced Range Telemetry (ARTM) waveforms. The overarching objective of the proposed research is to develop a low power, miniaturized, multi-frequency transmitter for intelligent missile flight test applications. The system will remotely relay telemetry da ...STTR Phase I 2017 Department of DefenseMissile Defense Agency