Opportunity ID: 281120

General Information

Document Type: Grants Notice
Funding Opportunity Number: CRANBAA16-004
Funding Opportunity Title: Plasma Combined Mass-Flux and Gas Species Sensor For Hypersonic Combustion Monitoring
Opportunity Category: Discretionary
Opportunity Category Explanation:
Funding Instrument Type: Grant
Category of Funding Activity: Science and Technology and other Research and Development
Category Explanation:
Expected Number of Awards: 1
Assistance Listings: 12.300 — Basic and Applied Scientific Research
Cost Sharing or Matching Requirement: No
Version: Synopsis 1
Posted Date: Jan 22, 2016
Last Updated Date:
Original Closing Date for Applications: Feb 29, 2016
Current Closing Date for Applications: Feb 29, 2016
Archive Date: Mar 30, 2016
Estimated Total Program Funding:
Award Ceiling: $5,000
Award Floor: $0

Eligibility

Eligible Applicants: Unrestricted (i.e., open to any type of entity above), subject to any clarification in text field entitled “Additional Information on Eligibility”
Additional Information on Eligibility:

Additional Information

Agency Name: NSWC CRANE – N00164
Description: Naval Surface Warfare Center, Crane Division is interested in receiving proposals for research aimed at the development of a sensor that utilizes a small contained amount of ionized gas to simultaneously measure mass-flux and gas species in high-speed, high-enthalpy flows that are endemic of hypersonic flight and SCRAM-jet propulsion. The sensor is based on the optical emission properties of a stable glow discharge or plasma. The use of the plasma sensor for mass-flux measurements has already been demonstrated1. It incorporates a high frequency (1MHz) AC discharge to ionize the gas between two closely spaced electrodes. The voltage drop across the discharge correlates with the time-dependent mass-flux, ρU. With an alternate design, the plasma sensor can also be used to measure static pressure. Recent experiments have examined the use of the plasma sensor for spectral analysis of the optical emission produced by the glow discharge. Results for combustion in both Ethylene and Propane indicate that the plasma sensor produces useful emission lines that can be used to measure temperature, density and possibly gas species. Utilizing the other attributes of the plasma sensor, these optical emission measurements could be performed simultaneously with mass-flux and/or pressure in a combined sensor suite. The proposed research seeks to further develop this capability.
Link to Additional Information:
Grantor Contact Information: If you have difficulty accessing the full announcement electronically, please contact:

Steven Junkins

Contract Specialist

Phone 8128548833
Email:steven.junkins1@navy.mil

Version History

Version Modification Description Updated Date

Folder 281120 Full Announcement-1 -> CRANBAA16-004 Plasma Combined Mass-Flux and Gas Species Sensor For Hypersonic Combustion Monitoring.pdf

Packages

Agency Contact Information: Steven Junkins
Contract Specialist
Phone 8128548833
Email: steven.junkins1@navy.mil
Who Can Apply: Organization Applicants

Assistance Listing Number Competition ID Competition Title Opportunity Package ID Opening Date Closing Date Actions
12.300 PKG00220599 Jan 22, 2016 Feb 29, 2016 View

Package 1

Mandatory forms

281120 RR_SF424_2_0-2.0.pdf

281120 RR_OtherProjectInfo_1_3-1.3.pdf

281120 RR_Budget10_1_3-1.3.pdf

Optional forms

281120 RR_FedNonFed_SubawardBudget10_10-1.2.pdf

281120 RR_KeyPersonExpanded_2_0-2.0.pdf

2025-07-09T08:33:18-05:00

Share This Post, Choose Your Platform!

About the Author: