Attachment_B_MACH_Abstract_Template.docx

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Materials Architectures and Characterization for Hypersonics (MACH)
Solicitation number
HR001119S0022
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HR001119S0022 MACH BAA

Abstract Template

Use of this template is mandatory for all abstract submissions to this BAA. This document must include all components described herein and must be submitted in .pdf, .odx, .doc, or .docx formats. All submissions must be written in English and all pages shall be formatted for printing on 8-1/2 by 11-inch paper with 1-inch margins and font size not smaller than 12 point. Font sizes of 8 or 10 point may be used for figures, tables, and charts.

Abstracts shall not exceed a maximum of 7 pages.

Page limit includes:
Page limit does NOT include:
All figures, tables, charts
Cover Sheet

Table of Contents

Abstract Summary slide

Bibliography (Optional)

Technical Papers

[PRIME ORGANIZATION LOGO]

HR001119S0022 Program Name

Abstract

Abstract Title

Proposer Organization

Technical Area

Technical Point of Contact (POC)
Name:

Mailing Address:

Telephone:

Email:

Administrative POC
Name:

Mailing Address:

Telephone:

Email:

Other Team Members (subcontractors and consultants), if known/applicable
Technical POC Name:

Organization:

Technical POC Name:

Organization:

Estimated Total Cost (Phase I & II)
$

Estimated Period of Performance

Identify any other solicitation(s) to which this concept has been proposed

Table of Contents

1.Abstract Summary Slide4
2.Goals and Impact4
3.Technical Plan4
4.Capabilities/Management Plan4
5.Cost and Schedule4
6.Bibliography (Optional)5

Source Selection Information – See FAR 2.101 and 3.104

HR001119S0022 Abstract 5

Abstract Summary Slide [Using the Abstract Summary Slide template provided as an attachment to the BAA, provide a summary in PowerPoint that effectively and succinctly conveys the main objective, key innovations, expected impact, and other unique aspects of the proposed project. Include the PowerPoint slide as a separate attachment to this document.]

Goals and Impact Summary of the technical approach and innovative claims for the proposed research. This section is the centerpiece of the abstract and should succinctly describe the uniqueness and benefits of the proposed approach relative to the current state-of-art alternate approaches.

· Describe the unique technical approaches and solutions being proposed, with particular emphasis on innovative claims and quantitative end-of-program performance goals

· Describe how the proposed quantitative performance goals compare to what has already been demonstrated for hypersonic systems and adjacent fields.

· Discuss the quantitative impact of the proposed work, particularly to platforms best suited to the proposed approach (e.g. boost-glide, scramjet)

Technical Plan Technical rationale and constructive plan for accomplishment of technical goals in support of innovative claims and deliverable production.

· Identify and quantify major technical risk elements and potential mitigations (both technical and schedule)

· Include a brief technical development plan and appropriate measurable milestones associated with the development effort.

· Provide the technical basis for the scalability of the approach in quantitative terms, including manufacturing rate, part size and thermal performance.

Capabilities/Management Plan [Provide a brief summary of expertise of the team, including subawardees and key personnel. While teaming arrangements do not need to be finalized at the time of abstract submission, mention of potential teaming/collaboration arrangements is highly encouraged. Identify a principal investigator for the project and include a description of the team’s organization including roles and responsibilities.]

Cost and Schedule [Provide a cost estimate for resources (e.g., labor, materials) and any subawardees over the entire program (Phase I + Phase II), broken down by Government Fiscal Year]

Bibliography (Optional) [Provide a brief (no more than 2 pages) bibliography with links to relevant papers, references, reports, resumes of key team members, etc.]

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