NASA SBIR 2021-I Solicitation

Proposal Summary


   
Proposal Number:          21-1- S3.08-2638
          
          
   
Subtopic Title:
      Command, Data Handling, and Electronics
          
          
   
Proposal Title:
      A Radiation Hardened, Digitally Controlled Single-Inductor Multiple-Output (SIMO) Buck Regulator
          
          

Small Business Concern

   
Firm:
          
Alphacore, Inc.
          
   
Address:
          
304 South Rockford Drive, Tempe, AZ 85281
          
   
Phone:
          
(480) 494-5618                                                                                                                                                                                
          

Principal Investigator:

   
Name:
          
Yu Long
          
   
E-mail:
          
yu.long@alphacoreinc.com
          
   
Address:
          
304 South Rockford Drive, AZ 85281 - 3052
          
   
Phone:
          
(480) 494-5618                                                                                                                                                                                
          

Business Official:

   
Name:
          
Esko Mikkola
          
   
E-mail:
          
engineering@alphacoreinc.com
          
   
Address:
          
304 S Rockford Dr, AZ 85281 - 0000
          
   
Phone:
          
(480) 494-5618                                                                                                                                                                                
          

Summary Details:

   
Estimated Technology Readiness Level (TRL) :                                                                                                                                                          
Begin: 2
End: 4
          
          
     
Technical Abstract (Limit 2000 characters, approximately 200 words):

Alphacore will design, fabricate and test a buck DC-DC converter that can directly convert voltages from 5V – 12V down to 900mV, while supporting at least 10A of current to the load. Our goal is 20A load current, a requirement for some of the most powerful FPGAs. The output voltage will be settable between 900mW and 3.3V. In this Phase I program, we will design a digitally controlled, high-efficiency, radiation hard, hybrid GaN/CMOS integrated single module SIMO DC-DC converter to meet these specifications. The developed converter will have a reduced component count, enabling reduced failure modes, lower PCB area and it includes over voltage protection, fault tolerance, load monitoring, and allows control and status monitoring by a remote power system controller. This solution includes all controller circuitry and drivers integrated in a single CMOS ASIC chip, as well as the GaN-based DC-DC converter’s power stage. The hybrid module will have a very small form factor, namely 20mm x 20mm x 6mm.

Alphacore’s SIMO POL converter will utilize CMOS based drivers and controllers for the GaN power stage. The driver and controller would be based on X-FAB’s latest XT018 process, a 0.18 µm modular high-voltage SOI technology. It combines the benefit of conventional SOI wafers with Deep Trench Isolation (DTI), those of a state-of-the-art six metal layers 0.18 µm process, and localized partial SOI for unique high-voltage super-junction (SJ) power transistors. Unlike traditional high-voltage LDMOS devices from conventional bulk or SOI CMOS processes, the unique high-voltage SJ DMOS power transistors with VDS breakdown voltage of 100V, 140V and 200V offered in XT018 have reduced conduction loss with the same silicon area, such that lower FOM is available for higher efficiency applications. The planar high-voltage SJ DMOS transistor also has significantly better radiation tolerance for both total ionizing dose effects and single event effects.

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

Multi-output POL converters such as Alphacore’s solution allows compact, cost-effective spacecrafts, such as nanosatellites, to deliver capabilities that traditionally require larger satellites. It can also be applied to support future heliophysics missions like AWE launching in 2022, PUNCH and TRACERS, both launching in 2023, and IMAP launching in 2024. Future outer planets instruments that may benefit include the Galaxy Evolution Probe, PICO, POEMMA.

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

Non-NASA applications for Alphacore’s solution include planned constellations of nanosatellites or CubeSats for hypersonic missile defense and the United States Space Force, commercial spaceflight companies like SpaceX and Blue Origin, and satellite-based weather, data and global intelligence companies like Planet Labs and Capella Space.

          
          
     
Duration:     6
          
          

Form Generated on 04/06/2021 12:10:26