Name: Mr. Jamie McKee

E-mail: jamie@stormimpact.net
Address: 7510 Heatherwood Lane, Dublin, OH 43017
Phone: (614) 935-2835

Estimated Technology Readiness Level (TRL) :

Begin: 4
End: 7
Technical Abstract (Limit 2000 characters, approximately 200 words):

The reliability of the electrical grid is a matter of both national security and qualify of life. The frequency

of weather-related outages are expected to increase due to climate change. Electrical utilities in the
United States spend over $70 billion annually on storm restoration. The number of outages and cost can
be significantly decreased with better information on vegetation risk near critical infrastructure and
assessing key vulnerabilities. Stormlmpact Inc. will use NASA Earth Observation data to build machine
learning (ML) vegetation growth and risk models that will allow electrical utilities to proactively prepare
for storms and improve their infrastructure resilience. We anticipate cost savings of 10% to 20% for
utility customers due to improved vegetation management efficiency. We will leverage these data to
provide enhanced StormlImpact prediction models and a new national power outage forecast model.
These innovations will greatly improve storm preparedness, optimize vegetation management, and

improve the resilience of the electrical grid in a changing climate.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

This proposal is responsive to the solicitation "Technologies Using NASA Data to Foster Climate
Resilience". The vegetation risk and power outage prediction innovations proposed here are relevant to
NASA’s Applied Sciences Program because they can provide insights into the impacts of weather-related
disasters, wildfire risks, and inform long-term planning to improve the resilience of U.S. infrastructure in

a changing climate.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

These vegetation management products will address a critical market gap by providing electrical utilities
of all sizes with accurate and cost-effective guidance to identify vegetation issues before they cause
outages. In addition, the power outage models can be used by Federal agencies, emergency
management organizations, NGOs and the private sector to assess power outage risk and optimize pre-
storm preparations.

Duration: 24



Name: Kathryn Carpenter

E-mail: kathryn@ceciliaenergy.com
Address: 211 Warren St #516 Newark New Jersey 0710
Phone: (973) 348-6736

Estimated Technology Readiness Level (TRL) :

Begin: 4
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

Our technology is microwave-assisted thermocatalytic decomposition of mixed waste plastic. In Phase I,

we proved our lab-scale system and demonstrated high effi

iency conversion of plastic to hydrogen gas
and solid carbon with high yields. In Phase Il we propose to scale-up our system with data to be used in
the design and modeling of our first commercial pilot-scale reactor system. The ultimate goal of this
Phase II work is to compile a full engineering package for our first pilot-scale reactor system to be
deployed on customer sites for treatment of their waste plastic with concomitant generation of hydrogen

and performance carbon.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

Processing of mission trash to recover hydrogen gas for fuel or atmosphere regeneration. Production of

performance carbon for Low Earth Orbit manufacturing. Support of In Situ Resource Utilization goals.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

Beneficial reuse of waste plastic. Hydrogen fuel production. Production of performance carbon for

semiconductors, solar power generation, energy storage, water treatment, composite materials, and

other uses.
Duration: 18
Proposal Summary: Crystal Sonic, Inc.
Topic Title: Low-Cost Photovoltaic Arrays for Space

Proposal Title: Reducing Cost of Space Photovoltaics via Sound-Assisted Substrate Reuse



Duration: 18

Proposal Summary: Turion Space Corp.

Proposal Information

Topic Title: Commercial Development of Active Debris Remediation (ADR) Services
Proposal Title: Low-Cost CubeSat for Active Removal of Sizable Space Debris Utilizing a Mothership
Architecture

Small Business Concern

Firm: Turion Space Corp.
Address: 9272 Jeronimo Rd, Suite 107c, Irvine, CA 92618
Phone: (678) 689-4592

Principal Investigator:

Name: Mr. William Figueiredo

E-mail: bfigueiredo@turionspace.com

Address: 9272 Jeronimo Rd, Suite 107c, Irvine, CA 92618
Phone: (951) 236-9442

Business Official:

Name: Mr. Tyler Pierce

E-mail: tpierce@turionspace.com

Address: 9272 Jeronimo Rd, Suite 107c, Irvine, CA 92618
Phone: (425) 205-7022

Summary Details:
Estimated Technology Readiness Level (TRL) :
Begin: 3

End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):


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

Dedicated payload and cargo return is one of the few remaining items left unsolved for CLD business
models to close. Companies and institutions looking to iterate quickly in the space environment need
fast Earth return. A human rated version of the Cargo Ferry may one day provide a solution for CLDs

necessitating an emergency Earth return solution.

Duration: 24

Proposal Summary: re:3D, Inc.

Proposal Information

Topic Title: Point-of-use Recycling for Optimized Space-Age Logistics
Proposal Title: On-Orbit Additive Manufacturing Using Recycled Waste

Small Business Concern

Firm: re:3D, Inc.
Address: 1100 Hercules Ave Ste 220, Houston, TX 77058
Phone: (512) 730-0033 EXT 22

Principal Investigator:

Name: Patrick Ferrell

E-mail: patrick@re3d.org

Address: 1100 Hercules Ave Ste 220, Houston, TX 77058
Phone: (720) 987-8500

Business Official:

Name: Samantha Snabes

E-mail: samantha@re3d.org

Address: 1100 Hercules Ave Ste 220, Houston, TX 77058
Phone: (832) 746-0922

Summary Details:


Substrate re-use of GaAs photovoltaic devices for space.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

A wide range of emerging next-generation semiconductor device technologies based on ‘wide bandgap"
semiconductors, including SiC, GaN, AIN and others. Applications include: power electronics for electric
vehicles, electric motors, photovoltaic inverters and more; RF communication devices; UVC-LED devices

for disinfection; Laser diodes and sensor applications and more,

Duration: 15
Proposal Summary: H3X Technologies Inc.
Topic Title: Electric and Hybrid Electric Systems for Unmanned Aerial Vehicle (UAV) and Aircraft
in the 1500 to 5000 Ibs size class
Proposal Title: System Level Testing of HPDM-30 - A 10 kW/kg Integrated Motor Drive for UAV and

Aircraft Electric Propulsionn

Firm: H3X Technologies Inc.

Address: 410 S Arthur Ave Louisville Colorado 80027

Phone: (952) 913-7232

Name: Mr. Max Liben

E-mail: max@h3x.tech

Address: 410 S Arthur Ave Louisville Colorado 80027

Phone: (917) 608-1164

Name: Mr. Jason Sylvestre

E-mail: jason@h3x.tech

Address: 410 S Arthur Ave Louisville Colorado 80027


Firm: Crystal Sonic, Inc.

Address: 311 W. Virginia Ave, Phoenix, AZ 85003
Phone: (617) 515-5031

Name: Dr. Arno Merkle

E-mail: arno@xtalsonic.com

Address: 311 W. Virginia Ave, Phoenix, AZ 85003
Phone: (617) 515-5031

Name: Dr. Arno Merkle

E-mail: arno@xtalsonic.com

Address: 311 W. Virginia Ave, Phoenix, AZ 85003
Phone: (617) 515-5031

Estimated Technology Readiness Level (TRL) :

Begin: 5
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

High substrate costs limit the proliferation of many next-generation semiconductor device applications,
such as high-efficiency GaAs-based photovoltaics for space applications, often consuming 50% of the
cell manufacturing cost. We propose a novel substrate re-use technology, known as Sonic Lift-off (SLO),
to drive down the costs of space photovoltaic manufacturing. SLO utilizes sound to separate thin
devices from their host substrate, leaving the remaining substrate available for multiple reuses. A key
milestone in the march towards commercialization is the ability to demonstrate the technology at
industrially relevant wafer diameters and on real-world functioning devices. In this proposal we plan to
build upon our successes to date in Phase I, moving from 4" wafer SLO feasibility to functioning 4"
device feasibility and optimization. For this effort, a new SLO alpha tool (‘Gen2’) will be built and

operated in order to demonstrate overall performance.

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


Turion Space Corp. proposes developing a CubeSat-based debris remediation strategy, whereby several
"Deorbiter" CubeSats are deployed from a carrier spacecraft to remove multiple debris objects from LEO
(600-1500km) in a single mission. The system's mothership will be a scaled adaptation of Turion's DROID
platform, currently undergoing development for Space Situational Awareness (SSA) and Rendezvous
and Proximity Operations (RPO) applications. The DROID mothership will be equipped with a gridded ion
thrust to ensure maximum AV, an RPO computer vision system and CubeSat deployer. The Deorbiters
will be designed based on an 12-16U form factor and emphasize commercial-off-the-shelf components
with flight heritage to accelerate development timelines, scale production, and lower the Deorbiter unit
costs with economies of scale. If a Deorbiter does not have sufficient AV to deorbit a debris object,
multiple can be deployed and used on the same object, enabling the architecture to scale to larger
debris, higher energy orbits, and reduced deorbit timeframes. In addition, each Deorbiter will operate
independently of the mothership and, if issues arise, can deorbit itself to avoid creating additional
debris. The architecture does not require additional hardware on the target object, such as docking
adapters or communication systems. In addition, alternative state-of-the-art ADR methods such as throw
nets, space-based lasers, the ion-beam shepherd, electrodynamic tethers, and robotic arms have
drawbacks due to highly complex system dynamics and increased risk of further debris generation. The
proposed mission architecture maximizes commercial utility because the mothership will collect SSA
data when not performing the debris removal missions, and the Deorbiter system can be used for

multiple commercial applications such as life extension.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

The proposed Low-Cost CubeSat for Active Removal of Sizable Debris Utilizing a Mothership
Architecture will address critical ADR needs for NASA by deorbiting non-operational US government
owned space objects. The proposed employment of the multi-use capabilities of the mothership and
Deorbiter CubeSats have the potential to enable ADR to become a viable and sustainable part of the
growing space economy, reducing the fiscal burden on NASA for development and deploying this
technology.

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

The proposed Low-Cost CubeSat for Active Removal of Sizable Debris Utilizing a Mothership
Architecture maximizes commercial utility because the mothership will collect SSA data when not
performing debris removal missions, and the Deorbiter can be used for multiple applications such as life
extension and orbit relocation, eventually ranging beyond LEO to MEO and GEO. However, if Deorbiter
CubeSats are not utilizing mothership deployer slots, last-mile orbit delivery for commercial CubeSat

customers can be performed.

Duration: 24

Form Generated on 09/20/2023


Phone: (714) 876-7102

Name: Vanessa Kuroda

E-mail: vanessa@outpost.space

Address: 1601 Colorado Ave, Santa Monica, CA 90404
Phone: (650) 336-8659

Name: Paul Tomko

E-mail: paul@outpost.space

Address: 1601 Colorado Ave, Santa Monica, CA 90404
Phone: (310) 906-0070

Estimated Technology Readiness Level (TRL) :

Begin: 3
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

Today's cost to go to ISS and back represents a high barrier to entry for the Low Earth Orbit (LEO)
economy. Commercial LEO Destinations (CLDs) as well as the International Space Station (ISS) are in
need of the ability to have rapid cargo downmass capabilities in order to iterate quicker and accelerate
their business. In this effort, Outpost Technologies Corporation (Outpost) will address this need and
develop the Cargo Ferry which is a rapid cargo downmass vehicle that will be used for both returning
cargo from commercial space stations as well as the ISS. Beneficial applications of our innovation
include Earth return of non-human cargo, scientific samples, small payloads, and important research.
Driving down the cost of Earth return would open the door to more throughput on the ISS National Lab

while also enabling the broader Low-Earth orbit economy to flourish.

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

The ISS is at stowage capacity, requiring tough decisions by the ISS program office each time a new
payload is manifested. By downmassing stowed cargo, more room is made for new science and R&D on
station. On-demand availability of the Cargo Ferry as a backup trunk payload ensures there will be no

empty trunk space on future missions.


NASA SBIR Ignite 2022-II Solicitation

Proposal Summary: Ampaire Inc

Proposal Information

Topic Title: Electric and Hybrid Electric Systems for Unmanned Aerial Vehicle (UAV) and Aircraft
in the 1500 to 5000 Ibs size class
Proposal Title: High Efficiency Powertrain for Hybrid Aircraft (HEPHA)

Small Business Concern

Firm: Ampaire Inc
Address: 3507 Jack Northrop Ave, Hawthorne, CA 90250
Phone: (617) 335-8162

Principal Investigator:

Name: Dr. Edward Lovelace

E-mail: ed@ampaire.com

Address: 3507 Jack Northrop Ave, Hawthorne, CA 90250
Phone: (617) 335-8162

Business Official:

Name: Dr. Edward Lovelace

E-mail: ed@ampaire.com

Address: 3507 Jack Northrop Ave, Hawthorne, CA 90250
Phone: (617) 335-8162

Summary Details:
Estimated Technology Readiness Level (TRL) :
Begin: 4

End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words):


Phone: (520) 838-9404

Name: Dr. Stanislau Herasimenka

E-mail: SH@Solestial.com

Address: 7700 South River Parkway, Tempe, AZ 85284
Phone: (520) 838-9404

Name: Luke Gordon

E-mail: LG@Solestial.com

Address: 7700 South River Parkway, Tempe, AZ 85284
Phone: (419) 549-0872

Estimated Technology Readiness Level (TRL) :

Begin: 4
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

Solestial, Inc. (formerly Regher Solar) in collaboration with Opterus Research and Development, Inc.
(Opterus) propose this SBIR Ignite Phase 2 project to continue development of a novel photovoltaic solar
array technology for large-scale spacecraft and planetary surface infrastructure that can overcome size,
cost and weight limitations of the existing solar array technologies, achieve >50 kWe scale, 200 W/kg
specific power and 50 kW/m3 stowed volume efficiency while simultaneously having $40/W cost and

>1,000 MW manufacturing potential.

The proposed innovation is based on the integration of the the next generation radiation hard and ultra-
light silicon solar blankets developed by Solestial with R-ROMA deployment system developed by
Opterus. The proposed Phase 2 project will focus on increasing the readiness of the blanket framing
system - the key technology required to integrate thin silicon blankets with R-ROMA deployment system.
A 500W framed blankets will be produced and tested to achieve TRL 6 followed by flying ona
commercial spacecraft to achieve TRL 7. The proposed Phase 2 project will also develop a model and
engineering drawings for a 15 kW solar array. Solestial will be offering a 15 kW array to commercial
customers and will be looking to build a flight model using follow on funding after 2025. Finally, Solestial

will be looking to build a full size 50 kWe solar array and fly it with commercial space station.


Estimated Technology Readiness Level (TRL) :

Begin: 2
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words):

re:3D Inc. proposes to build a functional benchtop demonstration unit of an integrated waste-to-print
recycling system based on a granulation mechanism and 3D printer capacble of turning thermoplastic
waste generated from logistics foam available from in-space applications into functional and useful
objects through the use of material extrusion additive manufacturing (AM). This will be a low size, weight
and power (SWaP) engineering prototype based on re:3D's commercial Gigabot X (GBX) technology and
new innovative methods to shred the bulk foam and transport the resulting loose granulate in a
contained system. The design will address the unique challenges of operating in microgravity with

limited space and power resources.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

NASA has specifically identified packaging materials as an upmass of significant logistical overhead,
and its reuse must be considered - particularly for lunar and deep space missions which have limited

opportunities for resupply and waste disposal.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

A waste-to-print system integrated in a small form factor would be of use to US Navy submarines on
active deployment which can be away from supply and repair opportunities for months at a time. This

development might also be of interest to individuals and families looking for a personal recycling

system.
Duration: 24
Proposal Summary: Solestial, Inc.
Topic Title: Low-Cost Photovoltaic Arrays for Space
Proposal Title: Next Generation Silicon Based Solar Arrays for Space Stations and Other Permanent
Space Infrastructure
Firm: Solestial, Inc.

Address: 7700 South River Parkway, Tempe, AZ 85284


Phone: (952) 913-7232

Estimated Technology Readiness Level (TRL) :

Begin: 5
End: 8
Technical Abstract (Limit 2000 characters, approximately 200 words):

The HPDM-30 is a ultra-high power density 30kW integrated motor drive (IMD) for Unmanned Aerial
Vehicle (UAV) and Small Aircraft Electric Propulsion. It combines the motor and inverter into a single unit
and utilizes the same advanced core technology developed for H3X's flagship product, the HPDM-250.
H3X is targeting a combined motor/inverter efficiency of 93% and a continuous specific power of 10
kW/kg, making it 3X more power dense than anything else commercially available. The goal of this Phase
Il proposal is to manufacture a full-scale HPDM-30 prototype in order to perform functional testing,

performance characterization, and baseline environmental testing of the full IMD system.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):
25% SUSAN Flight Research Vehicle (SARV), X-57

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

Unmanned Aerial Vehicles (UAVs), Underwater Vehicles (AUVs and ROVs), cargo drones, Auxiliary Power
Units (APUs) and onboard power generators, aerospace actuators, electric boats, light electric aircraft,

electric motorcycles, and specialized industrial applications.

Duration: 10

Proposal Summary: Outpost Technologies Corporation

Topic Title: Enabling technologies for the development of a robust Low-Earth Orbit Economy
Proposal Title: Outpost Cargo Ferry: A Rapid Cargo Downmass Vehicle
Firm: Outpost Technologies Corporation

Address: 1601 Colorado Ave, Santa Monica, CA 90404


The proposed RHAM addresses the major NASA strategic goal of enabling the commercial LEO

economy. The RHAM production system will reduce or fully remove the need for the costly machining of

reusable TPS materials and promote the commercial LEO economy, directly in support of NASA’s CLD
strategic vision. This will support many of NASA’s missions that now utilize spacecraft manufactured by

commercial companies, providing faster development and manufacturing which will lead to lower overall

costs for the administration.

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

The RHAM platform has attracted serious interest from commercial space companies and has significant
potential for near-term insertion into commercial missions. This spans across a variety of space verticals
that include reusable rockets, downmass logistics, orbital spacecraft, and hypersonics. Some specific
applications include Sierra’s Dreamchaser, SpaceX’s Starship, and NASA’s Orion capsule contracted to
Lockheed. Furthermore, there is strong alignment with military defense systems in development today
that can utilize reusable TPS.

Duration: 16
Proposal Summary: Cecilia Energy

Topic Title: Point-of-use Recycling for Optimized Space-Age Logistics

Proposal Title: Catalytic Conversion of Waste Plastic to Hydrogen and Performance Carbon
Firm: Cecilia Energy, inc.
Address: 211 Warren St #516 Newark New Jersey 07103
Phone: (973) 348-6736
Name: Kathryn Carpenter
E-mail: kathryn@ceciliaenergy.com
Address: 211 Warren St #516 Newark New Jersey 0710

Phone: (973) 348-6736



Proposal Summary: Terrafuse, Inc.

Proposal Information

Topic Title: Technologies Using NASA Data to Foster Climate Resilience
Proposal Title: Wildfire Mitigation through Explainable Risk Predictions

Small Business Concern

Firm: Terrafuse, Inc.
Address: 2261 Market Street, #5161 San Francisco California 941146
Phone: (707) 570-5450

Principal Investigator:

Name: Mr. Stephen Marshall

E-mail: steve@terrafuse.ai

Address: 8 Putnam Ave, Chelmsford, MA 11824
Phone: (617) 797-2172

Business Official:

Name: Hunter Connell

E-mail: hunter@terrafuse.ai

Address: 2261 Market Street, #5161 San Francisco California 94114
Phone: (707) 570-5450

Summary Details:
Estimated Technology Readiness Level (TRL) :
Begin: 4

End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

The proposed innovation is built upon and improve the wildfire explanation and mitigation prediction

capabilities developed in Phase | of this contract. Mitigations are actions like clearing defensible space


Address: 13539 Desmond St Pacoima California 91331

Phone: (818) 422-0514

Name: Mr. Alex Pilmer

E-mail: alexp@transastra.com

Address: 13539 Desmond St Pacoima California 91331
Phone: (626) 533-7233

Estimated Technology Readiness Level (TRL) :

Begin: 4
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

The increasing accumulation of orbital debris has become a critical challenge for space operations and
economic development of space, posing a significant threat to the safety and sustainability of the space
environment. To address this issue, TransAstra proposes to advance the design, testing, and
commercialization of its cutting-edge Apis Capture Bag technology. The Apis Capture Bag is derived
from technology originally envisioned for the Asteroid Redirect Mission. It utilizes inflatable booms to
deploy a rip-stop bag around the target debris. The bag fully seals before making contact with the target
and then retracts to secure the debris safely. This scalable, adaptable, and efficient debris capture, and
containment system is uniquely designed to tackle a wide range of debris removal missions, from small
satellites to large spent rocket bodies. The proposed program encompasses five key Task Areas,
focused on addressing the specific technical objectives of rotational dynamics management, capture
bag scalability, multi-target confinement, architectural modeling, and space-qualified payload maturation.

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

Primary applications are orbital debris removal, supporting mission safety and preserving the space
environment for future exploration endeavors. Additional NASA applications would be servicing, repair,
or refueling missions for current NASA spacecraft, enhancing operational capabilities and extending

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

The Apis Capture Bag provides commercial satellite operators with a robust debris removal solution,
ensuring compliance with their disposal plans. Furthermore, the capture bag system can be employed
for in-orbit servicing missions, supporting satellite life extension, maintenance, and refueling operations.


Phone: (301) 602-0456

Name: Will Dickson

E-mail: will@canopyaerospace.com

Address: 8101 Midway Drive Suite A Littleton Colorado 80125
Phone: (469) 585-4838

Estimated Technology Readiness Level (TRL) :

Begin: 3
End: 6
Technical Abstract (Limit 2000 characters, approximately 200 words):

NASA has a stated strategic goal to promote a commercial presence in LEO, as formalized in their
Commercial LEO Destinations (CLDs) program. Given the emphasis on transitioning to CLDs, highly
available thermal protection system (TPS) manufacturing has become an even more critical capability.
Unfortunately, reusable TPS materials such Alumina-Enhanced Thermal Barrier (AETB or “Shuttle Tile”)
developed for the Shuttle program are still the state-of-the-art option despite high costs, long lead times,

and incredible amounts of manual labor (~2 tiles/week per technician).

To fill this gap, Canopy Aerospace Inc. (Canopy) proposes to develop the Reusable Heatshields Additive
Manufacturing (RHAM) platform, that allows rapid production of reusable TPS tiles with digitally defined
tailorability. The proposed development of RHAM will leverage Canopy’s experience in advanced
manufacturing of thermal protection system materials. RHAM advantages are made possible by the
unique Canopy innovations that include: 1) New TPS material formulations that open up the space of
usable precursors and manufacturing routes; 2) Unique implementation of a state-of-art binder jetting
process to produce highly insulative ceramics; and 3) New heat treatment processes for forming
mechanically resilient porous ceramics.

Canopy’s Phase II RHAM project will mature the manufacturing approach, laying the foundation for
scalable production of high-performance reusable TPS materials. Phase II will culminate in simulated
reentry ground testing at the NASA Langley HyMETS facility, enabling an accurate performance
comparison between RHAM and legacy TPS materials. The HyMETS testing will secure readiness level
(TRL) 6 for the RHAM technology and indicate readiness for potential transition to both NASA and

commercial space companies.

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


Ampaire proposes to fabricate, integrate, and test a novel hybrid electric powertrain on Ampaire's
electrified propulsion flying testbed. The AMP Drive model AMP-H270 consists of a modern JetA/SAF
engine plus electric machine in a hybrid electric configuration to enable flexible implementation in a
number of aircraft applications. The JetA/SAF engine is a high efficiency compression ignition (Cl)
engine from subcontractor DeltaHawk (Racine, WI) that will be coupled to Ampaire’s custom electric
boost and regeneration system to provide several key features: enabling multi-mode hybrid electric
operation, and significant reduction in fuel use. The AMP Drive hybrid unit will replace a conventional lO-
550 avgas engine to power the tail propeller in Ampaire's hybrid Skymaster 337, and retain the all electric
nose propeller drive. The aircraft will be converted to be supplied by JetA and SAF and retain Ampaire's
high voltage lithium battery. Ground and flight testing will verify the performance and utility of the hybrid

powertrain technology for a range of potential future applications with NASA, DoD, and commercially.
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

Hybrid electric manned and unmanned aircraft applications including the NASA SUSAN roadmap.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

DoD unmanned and manned cargo and passenger applications and commercial applications in
Ampaire's roadmap with distributed electric propulsion.

Duration: 12 Months

Proposal Summary: Canopy Aerospace Inc.

Topic Title: Enabling technologies for the development of a robust Low-Earth Orbit Economy
Proposal Title: Reusable Heatshields Additive Manufacturing (RHAM)

Firm: Canopy Aerospace

Address: 8101 Midway Drive Suite A Littleton Colorado 80125

Phone: (301) 602-0456

Name: John Howard

E-mail: john@canopyaerospace.com

Address: 8101 Midway Drive Suite A Littleton Colorado 80125


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

The proposed technology will meet the NASA goal of bringing to TRL 6 by 2030 50 kW-scale photovoltaic
solar arrays, deployed vertically or horizontally, providing power at >200 V at 200 W/kg BOL and
exhibiting no more than 10% degradation over ten years in the Lunar polar environment. Large scale
arrays can also be used to power future science missions using solar electric propulsion as well as non-

nuclear deep space missions.
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

50 kW-scale solar arrays are needed for commercial space stations and solar electric propulsion tugs. In
addition to meeting 200 Wikg and 50 kW/m3 goals commercial customers are looking for at least 10X
cost reduction compared to the state of practice. The proposed technology can deliver $40/W
manufacturing cost making it the most cost effective solution on the market.

Duration: 18
Proposal Summary: StormImpact Inc.
Topic Title: Technologies Using NASA Data to Foster Climate Resilience
Proposal Title: Real-Time Vegetation Risk Integration in Utility Damage and Outage Modelling to
Improve Resilience of the Utility Grid to Extreme Weather
Firm: StormImpact Inc.
Address: 7510 Heatherwood Lane, Dublin, OH 43017
Phone: (614) 935-2835
Name: Dr. Brent McRoberts
E-mail: brent@stormimpact.net
Address: 7510 Heatherwood Lane, Dublin, OH 43017

Phone: (317) 847-2003



around buildings or installing fire-resistant vents. Explanations describe the relative importance of each
input to the wildfire prediction model, or feature, to the overall wildfire risk; we refer to these
explanations as feature contributions. Feature contributions will be used to create localized mitigation
guidance that will support more optimal resource allocation and better decision-making during pre-
wildfire planning for the insurance industry and the public.

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

This innovation is a show case for how NASA's space-based observing programs make a difference on
Earth. It makes extensive use of NASA data sets, such as the Shuttle Radar Topography Mission (SRTM),
the Moderate Resolution Imaging Spectroradiometer (MODIS), the Shuttle Radar Topography Mission
(SRTM), the NASA Global Fire Atlas, and Canopy and Anderson Fuel data sets from Land fire, developed
using NASA Landsat data.

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

This innovation is targeted at the insurance industry: society's first line of defense for coping with
wildfire damage. The insurance industry does not know how community and property-level mitigation
affects wildfire risk. This innovation will provide location-specific guidance on which mitigating actions
will be most effective.

Duration: 18

Proposal Summary: Trans Astronautica Corporation (TransAstra)

Topic Title: Commercial Development of Active Debris Remediation (ADR) Services
Proposal Title: ApisTM Capture Bags for Collection of Large Orbital Debris: Ground Test Bed
Demonstrations and Payload Commercialization

Firm: Trans Astronautica Corporation

Address: 11404 Camaloa Ave Sylmar California 91342
Phone: (818) 422-0514

Name: Dr. Joel Sercel

E-mail: joel@transastra.com