NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-1 S3.02-8954
SUBTOPIC TITLE: Propulsion Systems for Robotic Science Missions
PROPOSAL TITLE: High Performance Iodine Feed System

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Busek Company, Inc.
11 Tech Circle
Natick, MA 01760 - 1023
(508) 655-5565

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. James Szabo
jszabo@busek.com
11 Tech Circle
Natick, MA 01760 - 1023
(508) 655-5565

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Judy Budny
judy@busek.com
11 Tech Circle
Natick, MA 01760 - 1023
(508) 655-5565

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 4

Technology Available (TAV) Subtopics
Propulsion Systems for Robotic Science Missions is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
The proposed innovation is an advanced iodine feed system for Hall Effect Thrusters (HETs), ion engines, cathodes, and other plasma generators. This feed system features a low mass plastic propellant tank that may be manufactured through additive processes. This allows low cost, complex shapes that can maximize the use of available space inside the spacecraft. The feed system also features an innovative piezo valve that will save volume, mass, cost, and energy with respect to the state of the art alternative for iodine.
Iodine stores as a solid and sublimates as the molecule I2, which allows many benefits with respect to traditional Hall Effect Thruster fuels such as xenon and krypton. These advantages include higher storage density, lower storage pressure, the ability to test high power systems at space-relevant conditions in modest facilities, the capability to store propellant in space without active regulation, and the capacity to transfer propellant at low pressure conditions in space. In a space-limited spacecraft, the use of iodine instead of state of the art xenon could increase available delta V by a factor of 3 or more. Iodine is especially beneficial for small CubeSat sized spacecraft.
In Phase I, Busek will design a feed system featuring the new, advanced components. The system will then be demonstrated with an iodine fueled thruster in space relevant conditions. In Phase II, an improved feed system will be designed, built and tested.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed feed system supports iodine Hall thrusters, ion engines, hollow cathodes, and other plasma generators currently under development for NASA. Specific applications include iSat, Lunar Cube, and future Game Changing missions. The Phase II feed system will be ideally sized for a Hall thruster operating at 500 to 1000 W. This thruster would be used for orbit raising and interplanetary transfers of spacecraft up to several hundred kg. Missions of current interest include resource prospecting at the moon, Mars, asteroids, and NEOs. The technology is also applicable to much smaller spacecraft, such as CubeSats, and much larger spacecraft, such as future MW-class cargo transports supporting human exploration.
The ability to flow iodine as a HET propellant is ultimately the game changer. Iodine is efficient, compact, highly storable, and an order of magnitude cheaper than xenon. Full power thruster demonstrations and throttling in space conditions are feasible because iodine is efficiently pumped by liquid nitrogen cooled panels.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed feed system supports many types of plasma generators used in space and on the ground. In the near term, the innovative feed system components are most likely to be used as part of a space propulsion system. The next stage for commercial users is an all-electric satellite, where electric propulsion accomplishes all propulsion functions including orbit raising, orbit circularization, inclination changes, station-keeping and repositioning.
Beyond stored density and pressure, iodine has many additional benefits with respect to xenon. For instance, a fully-fueled, non-active system may be stored on the ground or on orbit for long periods of time. This reduces the cost of on-orbit spares, and minimizes down-time in the event of a failure. Low pressure on-orbit refueling is also feasible. Due to its these and other advantages, iodine may be very attractive for commercial missions such as asteroid mining.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Fuels/Propellants
Maneuvering/Stationkeeping/Attitude Control Devices
Material Handing & Packaging
Polymers
Pressure & Vacuum Systems
Prototyping
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)
Spacecraft Main Engine

Form Generated on 04-23-15 15:37