NASA SBIR 2019-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 19-1- S1.06-3761
SUBTOPIC TITLE:
 Particles and Fields Sensors & Instrument Enabling Technologies
PROPOSAL TITLE:
 Fast Transient Response High Voltage Power Converter for Space Applications
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
QorTek, Inc.
1965 Lycoming Creek Road, Suite 205
Williamsport, PA 17701- 1251
(570) 322-2700

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Dr. Gregory Bower
E-mail:
gbower@qortek.com
Address:
1965 Lycoming Creek Road, Suite 205 Williamsport, PA 17701 - 1251
Phone:
(570) 322-2700

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Cathy Bower
E-mail:
cbrooke@qortek.com
Address:
1965 Lycoming Creek Road, Suite 205 Williamsport, PA 17701 - 1251
Phone:
(570) 322-2700
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words)

The proposed program addresses the need for a high voltage converter capable of ultra-fast slew rates and be within a small satellite form factor.  The proposed innovation leverages a Class-E derived topology of converters by combining an RF source (inverter) and an impedance matched rectifier to produce high voltages at efficiencies greater than 95%.  These efficiencies are possible through the implementation of resonant switching in the topology.  In addition, by implementing power switching at the MHz to 10s of MHz , the size of the converter can be minimized through the requirement of needing smaller values capacitors and inductors (coreless).  The required modulator is also simplified in the Class-E design as the single power switch (GaN MOSFET technology) utilizes a ground reference source simplifying the gate driver requirements.  The modulator will also enable a means to control the output voltage to deliver a linear response to the input command.  The rectifier stage will satisfy a 25kV output isolation requirement needed by detection instruments.  The Phase I program will produce a 10kV high voltage supply with the converter implementing a scalable output rectifier such that additional rectifiers added on the output can be placed in series and boost the output voltage.  As the design matures, we intend to ensure that a path exists for all utilized components to have radiation hardened equivalents to achieve a future rad option.  At Phase I exit, we will have demonstrated a converter with rectifiers placed in series with the output to achieve the desired closed-loop regulated 10kV target. 

 

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

The subcompact-sized high performance radhard HV ultrafast slew rate (high power) supply offers significant impact to a wide range of NASA SmallSat missions including detection instruments, X-ray tube, gyroscopes, plasma initiators etc. by reducing existing HV power solutions by as much as 10×. The technology would significantly impact surface exploration missions by providing radhard power solutions greatly reducing size/weight of lander subsystems on such as Mars Science Laboratory.

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

QorTek is heavily engaged in both magnetic-based and piezo-based HV supply design and products. However, along with commercial space opportunities, the proposed new class-E derived RF HV supply fills an untapped market need for very small high performance HV supplies in wafer manufacture, aerospace, and defense systems needs such as sensor/detector high voltage modulator systems.

Duration: 6

Form Generated on 06/16/2019 23:16:23