Glide Breaker Phase 2

Closed Pre-Solicitation Posted

Solicitation number
HR001122S0036
Agency
Defense Advanced Research Projects Agency Department of Defense
Responses due
Set-aside
No set-aside

Opportunity facts

NAICS code
541715 Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)
PSC
AC13 National Defense R&D Services; Department Of Defense - Military; Experimental Development

Notice details come from SAM.gov. Updated .

About this opportunity

The Defense Advanced Research Projects Agency seeks proposals to conduct wind tunnel and flight testing to collect data on jet interaction effects between divert and attitude control jets and hypersonic cross flows at conditions relevant to a future glide-phase interceptor. Proposers are to design and test a Demonstration System payload to characterize jet interactions and quantify their effects to inform validation of models and designs for an operational interceptor concept utilizing such jets. Proposals are due by July 8, 2022 and will be evaluated based on scientific and technical merit, contribution to DARPA's mission, and realism of costs and schedule.

There is no set-aside designation for this opportunity. Relevant NAICS codes may include 336414 and 541715, while PSC codes C399 and R425 are applicable. No incumbent or current contractors are identified. Proposers are expected to deliver a full design data package for the demonstration system as well as update the conceptual design of a potential operational system incorporating knowledge gained during testing, with an anticipated single award of indefinite-delivery/indefinite-quantity type.

Notice text

This Glide Breaker Phase 2 funding opportunity seeks proposals to execute wind tunnel and flight testing to collect data on jet interaction effects between divert and attitude control jets and a hypersonic cross flow at conditions relevant to a future glide-phase interceptor for hypersonic threats. The results of this phase are intended to inform designs and model development to enable acquisition of an interceptor utilizing a divert-and-attitude-control-system-propelled kill vehicle in a future program of record.

Attachments

Files attached to this notice, newest first
File Type Posted
HR001122S0036-Amendment-01.pdf PDF
Glide_Breaker_Phase_2_QA_Final.pdf PDF
Attachment_2_Proposers_Day_Q_A.pdf PDF
HR001122S0036.pdf PDF
Attachment_1_DARPA_Standard_Cost_Proposal_Spreadsheet.xlsx XLSX spreadsheet

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