Opportunity Information: Apply for NNH15ZOA001N 15GCD C1
Apply for NNH15ZOA001N 15GCD C1
- The NASA Headquarters in the science and technology and other research and development sector is offering a public funding opportunity titled "Game Changing Development Program, Ultra Lightweightcore Materials For Efficient Load Bearing Composite Sandwich Structures Appendix" and is now available to receive applicants.
- Interested and eligible applicants and submit their applications by referencing the CFDA number(s): 43.009 Cross Agency Support.
- This funding opportunity was created on Oct 24, 2014 and posted on Oct 24, 2014.
- Applicants must submit their applications by Dec 16, 2014. (Agency may still review applications by suitable applicants for the remaining/unused allocated funding in 2026.)
- The number of recipients for this funding is limited to 10 candidate(s).
- Eligible applicants include: County governments.
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Opportunity Summary:
NASA Headquarters released this grant opportunity on October 24, 2014 as a focused appendix under the Space Technology Mission Directorate (STMD) NASA Research Announcement called Space Technology Research, Development, Demonstration, and Infusion 2015 (SpaceTech REDDI 2015). The specific appendix sits within the Game Changing Development (GCD) program and is identified as NNH15ZOA001N 15GCD C1, titled "Ultra Lightweight Core Materials for Efficient Load Bearing Composite Sandwich Structures." In practical terms, NASA used the broader SpaceTech REDDI 2015 umbrella solicitation and then posted this topic as a distinct appendix with its own technical goals and proposal requirements, all accessed through the NSPIRES system.
The core technical purpose is to mature and demonstrate scalable manufacturing methods for ultra-lightweight core materials that can serve as lower-mass substitutes for conventional honeycomb or foam cores used in composite sandwich structures. Composite sandwich structures are widely used in aerospace because they provide high stiffness and strength at relatively low weight, but the core material can still drive mass, cost, and manufacturability limits. NASA is looking for next-generation, hierarchical or advanced-architecture core concepts enabled by newer manufacturing techniques, with an emphasis on whether they can be produced at meaningful size and at a cost that makes them a realistic alternative rather than a lab curiosity. The desired end state is a set of processes and resulting core structures that can be produced as both flat panels and curved components, suitable for large-scale sandwich structures.
A key performance target spelled out in the appendix is that the resulting ultra-lightweight core structures should achieve half or less the areal density of conventional honeycomb cores while retaining mechanical properties that are equivalent or better. In other words, NASA is explicitly prioritizing major mass savings without trading away load-bearing capability. The work is framed around moving from promising manufacturing concepts to repeatable, scalable production approaches, and then proving those approaches through fabrication and testing of representative articles. The emphasis on both flat and curved forms signals NASA interest in real flight-like geometry and not just idealized coupons.
The acquisition strategy is phased, using a progressive competitive down-selection process. Phase I is described as a Manufacturing Feasibility phase, expected to last up to 13 months, and Phase II is a Scale Up and Test Article Fabrication phase, expected to last up to 18 months. Selection for later phases is not treated like a brand-new competition; instead, NASA expects to build on what is demonstrated in the earlier phase. The agency anticipates that the Phase I awardees will be the most likely to succeed in Phase II, and it plans to request Phase II proposals primarily from those Phase I contractors via request letters that outline what to submit and how it will be evaluated. Even with that expectation, NASA states that proposals from all responsible sources will be considered if they are submitted by the due date for the later phase, but those outside the earlier phase winners must essentially prove they are at the same level of design maturity. To be competitive for Phase II without having been in Phase I, an offeror must show maturity equivalent to Phase I awardees, provide Phase I-equivalent documentation, and provide the Phase I test samples required for government testing; missing any of those elements can result in the proposal being found unacceptable without further consideration.
From an administrative and submission standpoint, proposals had to be submitted electronically through NSPIRES by an authorized organizational representative (AOR). NASA points applicants to the main SpaceTech REDDI 2015 NRA instructions and to the NASA Guidebook for Proposers Responding to an NRA or CAN (May 2014 edition). The notice strongly encourages organizations to register in NSPIRES early, learn the system ahead of time, and submit well before the deadline to avoid last-minute compliance or upload problems. NASA also encourages interested parties to monitor NSPIRES or subscribe to notifications for updates, including appendix postings and any clarifications.
For questions, NASA provided an email address (HQ_STMD_GCDC1@mail.nasa.gov) for technical, programmatic, and procurement inquiries. Responses were to be provided by email and could also be rolled into an FAQ document associated with the appendix on NSPIRES, with anonymity preserved for those who submit questions. A named point of contact is also referenced for access issues and general help (Ryan Stephan, Program Executive, STMD Game Changing Development Program).
The opportunity is listed as a discretionary grant in the science and technology research and development category, with an expected number of awards of about 10 and CFDA 43.009 (Cross Agency Support). No cost sharing or matching is required. The posting date and creation date are both October 24, 2014, with an original and current closing date of December 16, 2014, and an archive date of January 15, 2015. Award floor and ceiling are shown as 0 in the listing, which typically means applicants need to rely on the full appendix text in NSPIRES for any real funding ranges, budgets, or phasing amounts rather than the summary fields.
Overall, the opportunity is best understood as NASA seeking teams that can take ultra-lightweight, architected core concepts and turn them into scalable, cost-effective manufacturing processes that produce structurally credible sandwich-core components, including curved shapes, with a clear quantitative goal of cutting areal density by at least half relative to conventional honeycomb while meeting or exceeding mechanical performance. The phased structure and down-select language also makes it clear NASA wanted evidence-driven progress, with Phase I proving feasibility and providing test samples, and Phase II focused on scaling up and fabricating larger, more representative test articles for validation.
Frequently Asked Questions (FAQs)
What is the official title and identifier for this NASA grant opportunity?
The focused appendix is titled "Ultra Lightweight Core Materials for Efficient Load Bearing Composite Sandwich Structures" and is identified as NNH15ZOA001N 15GCD C1. It was released by NASA Headquarters under the Space Technology Mission Directorate (STMD) Game Changing Development (GCD) program as part of the broader SpaceTech REDDI 2015 NASA Research Announcement (NRA).
When was this opportunity released and what were the key dates?
The posting/creation date is October 24, 2014. The original and current closing date is December 16, 2014, and the archive date is January 15, 2015.
Where does this appendix fit within NASA solicitations?
This topic is a distinct appendix released under the broader umbrella solicitation called Space Technology Research, Development, Demonstration, and Infusion 2015 (SpaceTech REDDI 2015). NASA used the umbrella NRA for overarching instructions and then provided this topic as a focused appendix with its own technical goals and proposal requirements.
Where do applicants access the full appendix requirements and submit proposals?
Access and submission are handled through NSPIRES. NASA indicates that the appendix and related materials (including any posted clarifications and FAQs) are available through NSPIRES, and proposals had to be submitted electronically through that system.
What is the main technical goal of this opportunity?
The main goal is to mature and demonstrate scalable manufacturing methods for ultra-lightweight core materials that can replace conventional honeycomb or foam cores used in composite sandwich structures, while remaining structurally credible for load-bearing applications.
What types of structures is NASA focused on for these core materials?
NASA is focused on core materials for composite sandwich structures. The desired end state includes processes and resulting core structures that can be produced as both flat panels and curved components suitable for large-scale sandwich structures.
What kinds of core concepts is NASA interested in?
NASA describes interest in next-generation, hierarchical or advanced-architecture core concepts enabled by newer manufacturing techniques. The emphasis is on concepts that can move beyond laboratory demonstrations into repeatable, scalable production at meaningful size and realistic cost.
Is there a specific quantitative performance target for the core materials?
Yes. A key target is that the ultra-lightweight core structures should achieve half or less the areal density of conventional honeycomb cores while retaining mechanical properties that are equivalent or better.
Does NASA require that the new core materials match load-bearing performance?
Yes. NASA explicitly prioritizes major mass savings without trading away load-bearing capability, stating that mechanical properties should be equivalent to or better than conventional honeycomb cores while meeting the areal density reduction target.
What does NASA mean by "scalable manufacturing" in this context?
Based on the appendix description, NASA is looking for manufacturing approaches that can be repeated reliably, scaled to meaningful sizes, and used to produce both flat and curved core components. The objective is to demonstrate production approaches that are practical alternatives rather than one-off lab results.
What is the acquisition or award strategy for this opportunity?
The strategy is phased with a progressive competitive down-selection. Phase I focuses on Manufacturing Feasibility, and Phase II focuses on Scale Up and Test Article Fabrication. NASA expects later phases to build on evidence and results from earlier phases.
How long are Phase I and Phase II expected to last?
Phase I (Manufacturing Feasibility) is expected to last up to 13 months. Phase II (Scale Up and Test Article Fabrication) is expected to last up to 18 months.
How will Phase II proposals be requested and evaluated?
NASA anticipates requesting Phase II proposals primarily from Phase I contractors via request letters that outline what to submit and how proposals will be evaluated, reflecting NASA's expectation that Phase I performers are most likely to succeed in Phase II.
Can an organization participate in Phase II if it did not receive a Phase I award?
Yes, NASA states that proposals from all responsible sources will be considered if submitted by the Phase II due date. However, offerors that did not participate in Phase I must demonstrate a design maturity level equivalent to Phase I awardees and meet additional documentation and sample requirements described in the appendix summary.
What must a non-Phase I offeror provide to be competitive for Phase II?
To be competitive for Phase II without having been in Phase I, an offeror must show maturity equivalent to Phase I awardees, provide Phase I-equivalent documentation, and provide the Phase I test samples required for government testing. NASA indicates that missing any of these elements can result in the proposal being found unacceptable without further consideration.
How many awards did NASA expect to make?
The opportunity listing indicates an expected number of awards of about 10.
What type of funding opportunity is this listed as?
It is listed as a discretionary grant in the science and technology research and development category.
Is cost sharing or matching required?
No. The listing states that no cost sharing or matching is required.
What is the CFDA number associated with this opportunity?
The listing provides CFDA 43.009 (Cross Agency Support).
Why do the award floor and ceiling appear as 0 in the listing?
The summary fields show an award floor and ceiling of 0, which typically indicates that applicants should rely on the full appendix text in NSPIRES for actual funding ranges, budgets, and phasing amounts rather than the high-level summary fields.
What proposal instructions apply to this appendix?
NASA points applicants to the main SpaceTech REDDI 2015 NRA instructions and to the NASA Guidebook for Proposers Responding to an NRA or CAN (May 2014 edition). The appendix sits under the umbrella solicitation but carries its own technical goals and proposal requirements.
Who is allowed to submit the proposal in NSPIRES?
Proposals had to be submitted electronically through NSPIRES by an authorized organizational representative (AOR).
What administrative advice does NASA give about NSPIRES submission?
NASA strongly encourages organizations to register in NSPIRES early, learn the system ahead of time, and submit well before the deadline to avoid last-minute compliance issues or upload problems. NASA also encourages monitoring NSPIRES or subscribing to notifications for updates and clarifications.
How can applicants ask questions about the opportunity?
NASA provided the email address HQ_STMD_GCDC1@mail.nasa.gov for technical, programmatic, and procurement inquiries. Responses were to be provided by email and could also be incorporated into an FAQ document associated with the appendix in NSPIRES, with anonymity preserved.
Is there a named point of contact referenced for help?
Yes. The notice references Ryan Stephan (Program Executive, STMD Game Changing Development Program) for access issues and general help.
What kind of evidence is NASA looking for across the phases?
The appendix description emphasizes evidence-driven progress: Phase I is positioned to prove manufacturing feasibility and provide test samples, while Phase II is positioned to scale up and fabricate larger, more representative test articles for validation, including consideration of flat and curved forms.
Does NASA emphasize cost and manufacturability as evaluation considerations?
Yes. The description highlights an emphasis on whether the core concepts can be produced at meaningful size and at a cost that makes them realistic alternatives, not just laboratory demonstrations.
Does the opportunity specify interest in flight-like geometry?
Yes. The emphasis on producing both flat panels and curved components signals interest in real, flight-like geometry rather than only idealized coupon-level demonstrations.
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