One of nasas strategic goals is expanding scientific understanding of the earth and the universe. NASA envisions a broad class of scientific missions where extremely fine pointing and positioning of…

Ended Grant For Research Awarded Last action

Contract number
NNX16AL26G
Awardee
Awarding agency
Obligated
$493,461

Award facts

Contract value 100% obligated
$493,460.65 Current and potential, with all options
Completion date 100% complete
Current and potential, with all options
NAICS code
Not on record
Set-aside
No set-aside
Competition
Full and Open Competition · 0 offers Basic Research
Pricing
Other
Place of performance
Rolla, MO 65409, USA

Award details come from SAM.gov/FPDS.

Transactions

Action Obligated Date
Funding Only Action 5 -$5,403
Funding Only Action 4 $49,618
Other Administrative Action 3 $0
Other Administrative Action 2 $0
Funding Only Action 1 $200,000
Original award $249,246

About this award

This federal contract award, valued at $493,460.65, was issued by the National Aeronautics and Space Administration (NASA) to the University of Missouri System, doing business as Missouri University of Science & Technology (Missouri S&T). The contract is for a Phase II study to incorporate system-level issues and experimental results to validate and refine model predictions for plasmonic force propulsion, which can provide improved proximity and attitude control for small spacecraft, enabling new NASA science and exploration missions. This award is part of NASA's efforts to expand scientific understanding of the Earth and the universe through advanced spacecraft capabilities. The contract does not have a set-aside designation. As a leading technological research university, Missouri S&T leverages its expertise in areas such as aerospace engineering and materials science to support federal agencies like NASA through both contract and grant awards.

Description

One of nasas strategic goals is expanding scientific understanding of the earth and the universe. NASA envisions a broad class of scientific missions where extremely fine pointing and positioning of spacecraft is required, such as a single earth observing spacecraft, deployable x-RAY telescopes, exoplanet observatories, and constellations of spacecraft for earth and deep space observations. In recognizing this, the national research council emphasized the need for micro-propulsion for extremely fine pointing and positioning of micro-satellites for astrophysics missions. But the full potential of these small spacecraft remains untapped because they lack maneuverability. Plasmonic force propulsion provides attitude control capability for small spacecraft with minimal power penalty and minimal mass and volume penalty. Phase i results estimate a 1-2 order of magnitude improvement over the state-of-the-art in small spacecraft proximity and pointing precision control, creating new capabilities for small spacecraft enabling NASA science and exploration missions that were previously impossible. The goal of our phase II study is to incorporate system-level issues (i.e., thrust noise, thermal management, thrust throttling, off-axis illumination, and plasmonic effect sensitivity) and experimental results from demonstration of nanoparticle expulsion to validate/refine our model predictions. By including these issues in our analysis our goal is to show that plasmonic space propulsion can provide the level of proximity and attitude control envisioned for future NASA nano/picosatellite missions, a level that is better than state-of-the-art approaches. Our objective is to compare higher fidelity proximity/translational and attitude control predictions for plasmonic space propulsion with state-of-the-art approaches. Specific improvementsto the fidelity of our predictions include (1) incorporation of experimental plasmonic force measurements, (2) incorporation of thermal, e & m, and vibration effects on the plasmonic effect sensitivity, and (3) incorporation of off-axis illumination. Our approach is to couple results from experiments and sub-system models to quantify key propulsion metrics (noise, throttleability, etc.) and the corresponding effect of those metrics on precision pointing and attitude control of a nano/picosatellite. We will RE-evaluate mass, volume, and power requirements for plasmonic propulsion incorporating our refined assumptions, and compare with other state of-the-art control techniques. This approach to phase II builds off the approach, models and analysis of phase i. We will create a technology development roadmap, considering cost, risk, performance, and development time of key technologies. Our team is composed of experts in plasmonics, space propulsion, and astrodynamics. The proposed plan of work can be achieved within the proposed schedule because the proposed tasks build upon existing models and simulation tools already available to US. While the focus of the project is plasmonics for space propulsion, the proposed research will have wider application and relevance to optical nanotechnology with many non-aerospace spin-offs, such as plasmonic solar cells, thermoplasmonics for cancer thermal therapy, compact biological sensors, and photonic integrated circuits for optical communications. Plasmonics is an exploding new field of science and technology that is rapidly impacting every facet of optics and photonics, and is predicted to be one of the highest impact fields of the 21ST century.

Quick answers

Who was awarded contract NNX16AL26G?

NNX16AL26G was awarded to University Of Missouri System by Shared Services Center (National Aeronautics and Space Administration) on August 1, 2016.

How much is contract NNX16AL26G worth?

The government has obligated $493,461 on NNX16AL26G.

Was contract NNX16AL26G competed?

The extent of competition for NNX16AL26G was full and open competition. The government received 0 offers.

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