Upper Elevon Heater Carriage Fabrication

The document outlines the design and specifications for an Upper Elevon Dolly C Channel, designated 1JYR2-FLL-HPROJ-0091, for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. Key specifications include material (Steel ASTM A36 C-CHANNEL C6x8.2), finish requirements (primer and two coats of OSHA Safety Blue polyurethane), and human-readable identification marking. The document also includes detailed dimensional tolerances and notes on burrs and sharp edges. It emphasizes compliance with ASME Y14.100 for drawing interpretation and MIL-DTL-18264, MIL-PRF-23377, MIL-PRF-85285, and MIL-STD-130 for finishes and markings. The file is designated as EAR99/NLR, indicating no license is required for export, but it is subject to embargo regulations. The document was approved for initial release on November 10, 2025, with various approvals from NASA personnel.

This document from the National Aeronautics and Space Administration (NASA), Armstrong Flight Research Center, Edwards, California, details the design and specifications for an "UPPER ELEVON ROOT LIFTING CLEVIS." The document, identified as DWG. NO. FLL-HPROJ-0089, includes engineering drawings, revision history, and material/finish specifications. Key details include a primer/top coat finish per MIL-DTL-18264 and MIL-PRF-85285, material specified as A36 Steel Stock per ASTM A36/A36M, and human-readable identification marking per MIL-STD-130. The document also contains an EAR99/NLR notice, indicating that the information is technical in content but not restricted by ITAR or EAR regulations, classifying it as EAR99/NLR (No License Required) for export control purposes, with general prohibition six (embargo) still applicable. The design was approved for initial release on November 5, 2025, and reviewed/checked by multiple engineers.

This government file from the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center details the fabrication of an "Upper Elevon Carriage Frame." The document, identified as FLL-HPROJ-0049, specifies the materials, dimensions, and assembly instructions for various components of the carriage frame, including legs, angles, plates, washers, and crush tubes made primarily from HSS steel (ASTM A500/A500M) and A36 steel stock (ASTM A36/A36M). It outlines welding procedures (AWS D1.1/D1.1M with E7018 SMAW), visual inspection criteria, non-destructive testing (magnetic particle and dye penetrant), and finishing requirements (MIL-DTL-18264 primer/topcoat). The file also includes human-readable identification marking specifications (MIL-STD-130) and an EAR99/NLR notice regarding export control, confirming the technical content is not restricted by ITAR or EAR. Various diagrams detail the assembly steps and individual component specifications.

This document outlines the fabrication of a root frame for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It details the materials, specifications, and procedures required for welding, finishing, and identification marking of various root frame components, including eight distinct root frame legs and numerous washers, spacers, and a crush tube. Key specifications include welding according to AWS D1.1/D1.1M with visual, magnetic particle, and dye penetrant NDT, and a primer/top coat finish per MIL-DTL-18264. The document also provides detailed drawings and dimensions for each part, along with an EAR99/NLR notice regarding export control. The entire process is approved by NASA personnel, with specific dates for design, drawing, engineering, checking, and review.

This government file from the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center details the design and specifications for an "Inboard Reflector Frame" (DWG. NO. FLL-HPROJ-0046). The document, approved in December 2025, includes a comprehensive parts list, engineering drawings, and manufacturing notes. Key components include various steel legs, angles, crush tubes, spacers, and washers, all conforming to specific ASTM material standards. Manufacturing instructions outline welding procedures per AWS D1.1/D1.1M, primer/top coat finish per MIL-DTL-18264 (OSHA Safety Blue), and human-readable identification marking per MIL-STD-130. The document also contains an EAR99/NLR notice, indicating the information is technical but not subject to ITAR or EAR technology definitions, with embargo restrictions still applicable. The file includes detailed isometric, top, and bottom views of the frame and its individual components, along with dimensional tolerances and weldment steps.

This government file from the National Aeronautics and Space Administration (NASA), Armstrong Flight Research Center, details the design and specifications for an "OUTBOARD REFLECTOR FRAME." The document, identified as FLL-HPROJ-0047, includes an extensive parts list with materials such as HSS steel and A36 steel angles and rods, along with quantities required for each component. It outlines critical manufacturing processes, including welding specifications per AWS D1.1/D1.1M with specific visual inspection, magnetic particle, and dye penetrant NDT criteria. The file also specifies a two-coat primer/top coat finish per MIL-DTL-18264 and MIL-PRF-23377/MIL-PRF-85285, requiring OSHA Safety Blue (Color 15092). Human-readable identification marking per MIL-STD-130 is mandated. The document further includes detailed engineering drawings and notes on tolerances, dimensions, and projections, emphasizing no scaling of drawings and adherence to ASME Y14.100. It also contains an EAR99/NLR notice, indicating that the information is technical in content but not subject to ITAR or EAR technology definitions, thus requiring no export license, but with general prohibition six (embargo) still applicable. The file is approved by multiple engineers and reviewers, with drawing dates of November 24, 2025, and review dates of December 23, 2025.

This document, FLL-HPROJ-0101, details the specifications for “Kuchemann Angles” for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It outlines precise dimensions, materials, and finishing requirements. Key details include the use of A36 steel L angles, specific primer and topcoat finishes per MIL-DTL-18264 and MIL-PRF-23377/85285 standards, and human-readable identification marking per MIL-STD-130. The document also includes critical export control warnings, restricting transfer to foreign persons without specific approval. This technical drawing and its associated notes are essential for manufacturing these components, ensuring compliance with NASA's stringent engineering and regulatory standards. Review and approval dates indicate the document's official release and validation.

The document is a technical drawing titled "UPPER ELEVON ROOT LIFTING LINK" from the National Aeronautics and Space Administration (NASA), Armstrong Flight Research Center. It details the design, material specifications, and finishing requirements for a component identified as FLL-HPROJ-0088. Key specifications include A36 steel stock material, a primer/top coat finish per MIL-DTL-18264 and MIL-PRF-85285 (OSHA Safety Blue), and specific dimensional tolerances. The document includes detailed views of the link, revision history, approval dates, and an export control notice classifying the information as EAR99/NLR, meaning no license is required for export, but general prohibitions on embargoed countries apply. The drawing also specifies that parts shall be free of burrs and sharp edges, and holes must be masked prior to painting.

This document is a technical drawing for the "UPPER ELEVON OUTBOARD REFLECTOR FRAME BRACKETS" for the NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA), Armstrong Flight Research Center. It outlines detailed specifications for manufacturing, including dimensions, material (1/4" A36 Steel Stock), and finishing requirements (primer and topcoat per military specifications, OSHA Safety Blue color). The drawing also specifies identification marking instructions and lists approvals from various NASA personnel. Importantly, the document includes an EAR99/NLR notice, classifying the information as technical in content but not restricted by ITAR or EAR for export, with a reminder about general prohibitions related to embargoes.

This document is a technical drawing for the "Upper Elevon Inboard Reflector Frame Bracket" for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It details the design, material specifications, and finishing requirements for the bracket, which is made of 1/4" A36 Steel Stock per ASTM A36/A36M. Key specifications include precise dimensions, tolerances, and a primer/top coat finish per MIL-DTL-18264 and MIL-PRF-85285, using OSHA Safety Blue color. The document also outlines human-readable identification marking requirements and is designated as EAR99/NLR, indicating it is not subject to export license requirements under most circumstances, but still subject to embargo regulations. The drawing was approved by multiple NASA engineers in November 2025.

The National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center has released detailed engineering drawings for "Upper Elevon Axis Alignment Rods," identified as FLL-HPROJ-0085. The document specifies manufacturing requirements, including materials, dimensions, and finishes for three types of alignment rods: root, inboard, and outboard. Key specifications include primer and topcoat finishes per MIL-DTL-18264 and MIL-PRF-85285, material sourcing from specific part numbers (7767T52 and 7767T48), and human-readable identification marking per MIL-STD-130. The document also includes an EAR99/NLR notice, indicating that the information is technical in content but not subject to ITAR or EAR technology definitions, with an embargo clause for certain countries. The drawings are approved by multiple engineers and reviewers, with revision history details provided. These detailed plans are crucial for the precise fabrication of components for NASA's flight research projects.

The document outlines the design and specifications for the "UPPER HEATER ROOT LOCKING PLATE" assembly, designated FLL-HPROJ-0075, developed by the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. This technical drawing details the components, materials, manufacturing processes, and finishing requirements for the locking plate. Key components include the locking plate base, locking plate pin, and spacer plate, all made from A36 steel stock or rod per ASTM A36/A36M. The document specifies welding procedures in accordance with AWS D1.1/D1.1M, including visual, magnetic particle, and dye penetrant non-destructive testing. Finishing requirements involve a primer/top coat system per MIL-DTL-18264, using MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane, with specific masking instructions. Human-readable identification marking per MIL-STD-130 is also required. The document also includes an EAR99/NLR notice, indicating that the information is technical in content but not restricted by ITAR or EAR for export, though General Prohibition Six (Embargo) still applies. Detailed engineering approvals and revision history are provided, along with precise dimensional tolerances and views of the assembly and individual components.

The document is a technical drawing package for an "ELEVON WATER MANIFOLD BRACKET" (DWG. NO. FLL-HPROJ-0074) for the NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA), Armstrong Flight Research Center. It details the design, materials, and manufacturing specifications for the bracket and its components, the Water Manifold Base and Water Manifold Stiffener. Key specifications include welding per AWS D1.1/D1.1M, a primer/top coat finish per MIL-DTL-18264 (epoxy primer and polyurethane topcoat in OSHA Safety Blue), and human-readable identification marking per MIL-STD-130. The document also includes an EAR99/NLR notice, indicating that the information is technical in content but not restricted by ITAR or EAR, thus requiring no export license, with the caveat that General Prohibition Six (Embargo) still applies.

The document details the fabrication and assembly of the KUCHEMANN FRAME, a component for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It outlines the design, materials, and manufacturing processes, including specific welding, finishing, and identification marking requirements. Key components are the reflector frame base and stiffener, both made from A36 steel sheet. The document specifies the use of self-locking nutplates and solid rivets for assembly. It further provides detailed instructions for welding according to AWS D1.1/D1.1M, applying primer and topcoat finishes per MIL-DTL-18264 and MIL-PRF-85285, and permanent identification marking per MIL-STD-130. Rivet installation must comply with NASM47196. The file includes detailed engineering drawings with dimensions, tolerances, and revision history, and is designated as EAR99/NLR, indicating no license required for export, with embargo restrictions noted.

The document details the design and specifications for "ELEVON AXIS FEATURES" by NASA's Armstrong Flight Research Center. It includes engineering drawings, a parts list, and manufacturing notes for components such as the Root Hinge Line Axis Base and Rod Axis, and In/Outboard Rod Axis and Axis Base. Materials specified are 1045 Carbon Steel Plate and Rod, along with 1/2-20" HELICOIL inserts. Manufacturing instructions cover surface roughness, welding per AWS D1.1/D1.1M, primer/top coat finish per MIL-DTL-18264 and MIL-PRF-85285, helical coil insert installation per NASM33537, and identification marking per MIL-STD-130. The document also includes an EAR99/NLR notice, indicating it's technical but not controlled under ITAR or EAR, with embargo restrictions still applicable.

This document, FLL-HPROJ-0052, details the fabrication of a "LIFTING BAR" for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It includes engineering drawings and a parts list for the assembly, which consists of a lifting bar tube, linear bearing attachment plates, link clevises, and a lifting point plate, all made from specified steel materials. The document outlines critical manufacturing processes, including welding per AWS D1.1/D1.1M standards, primer/top coat finishing per MIL-DTL-18264 with OSHA safety blue polyurethane, and human-readable identification marking per MIL-STD-130. The design, drawn by N. Bierschwal and approved by multiple NASA personnel, is designated as EAR99/NLR, indicating it is not subject to ITAR or EAR technology definitions but is still subject to embargo provisions. The comprehensive nature of the document suggests its use in a federal government RFP for the manufacturing and delivery of this specialized lifting equipment.

The document details the design and specifications for Elevon Actuator Mounts, identified as FLL-HPROJ-0051, for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. It includes engineering drawings, a parts list, and manufacturing notes for three specific actuator mount types: Inboard, Outboard, and Root. The parts list specifies materials such as A36 steel channels and plates, with detailed dimensions and quantities. Manufacturing requirements include welding per AWS D1.1/D1.1M, primer/top coat finishes (MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane in OSHA Safety Blue or Gloss White), and human-readable identification marking per MIL-STD-130. The document also contains an EAR99/NLR notice, indicating that the information is technical in content but not restricted by ITAR or EAR, though subject to embargo provisions.

This government file, FLL-HPROJ-0050, details the fabrication of an Elevon Dolly for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. The document outlines the design, materials, and manufacturing specifications for the dolly, which includes an H-bar, expansion plates, and stiffener plates made from A992 and A36 alloy steel. Key requirements involve surface roughness, welding per AWS D1.1/D1.1M standards, and a specific primer/top coat finish using MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane. Identification marking must follow MIL-STD-130. The file includes detailed drawings and views for fabrication, ensuring compliance with specified dimensions and tolerances. The document is designated as EAR99/NLR, indicating No License Required for export, but subject to embargo provisions.

The document, FLL-HPROJ-0100, is a detailed technical drawing package from the National Aeronautics and Space Administration (NASA), Armstrong Flight Research Center, for the "UPPER ELEVON ROOT HINGE HINGE LINE BRACKETS." It includes engineering drawings, a parts list, and manufacturing notes for fabricating weldments used in aerospace applications. The project specifies the use of 1/2" A36 steel stock, welding procedures per AWS D1.1/D1.1M with E7018, and specific primer and topcoat finishes (MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane in OSHA Safety Blue). The document also outlines human-readable identification marking requirements per MIL-STD-130. All approvals, including design, check, and review, were completed in November 2025. The document is classified as EAR99/NLR, indicating No License Required for export, but notes that General Prohibition Six (Embargo) applies.

This document, a detailed engineering drawing from the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center, specifies the design and manufacturing requirements for "UPPER ELEVON ACTUATOR CLEVISES." It outlines critical dimensions, tolerances, materials, and finishing processes for these components. Key specifications include the use of 1018 steel per ASTM A106, specific primer and topcoat finishes (MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane in OSHA Safety Blue or Gloss White), and human-readable identification marking per MIL-STD-130. The document also includes an EAR99/NLR notice, indicating that the information is technical in content but not restricted by ITAR or EAR for export, though general prohibitions against embargoed countries still apply. The drawing provides detailed views, including root clevis and in/outboard clevis details, with various dimensions and thread specifications. Approvals from multiple NASA personnel and a revision history are also included.

The National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center in Edwards, California, has released a document detailing the "HEATER LINEAR RAIL HOUSING" (DWG. NO. FLL-HPROJ-0097). This document, dated November 10, 2025, outlines the design, materials, and manufacturing specifications for a critical component within the FLL-HPROJ-0059 assembly. Key specifications include the use of 1/4" A36 steel stock for the base plate and 2" OD A36 steel rod for the housing ring, both conforming to ASTM A36/A36M. The document details welding procedures per AWS D1.1/D1.1M using SMAW with E7018, visual inspection criteria, and non-destructive testing (NDT) including magnetic particle and dye penetrant. Finishing requirements specify a primer/top coat per MIL-DTL-18264, including MIL-PRF-23377 epoxy primer and MIL-PRF-85285 polyurethane in gloss white. Human-readable identification marking per MIL-STD-130 is also required. The document includes detailed drawings for both the base plate and housing ring, along with revision history, approvals, and an EAR99/NLR notice, indicating it contains technical content but is not ITAR- or EAR-controlled technical data, with general export restrictions applying.

This document, FLL-HPROJ-0096, from the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center, Edwards, California, details the design and specifications for an "UPPER HEATER LINEAR RAIL." The document includes engineering drawings, revision history, and approval dates, indicating it is a technical design file. Key specifications include material requirements (part number 6061K67, CAGE CODE 3A054) and identification marking instructions per MIL-STD-130. The design incorporates specific dimensions, tolerances (in inches), and notes regarding shaft stock and burr removal. The document also contains an EAR99/NLR notice, classifying the information as technical but not regulated by ITAR or EAR for export control, though it notes general export prohibitions still apply. The detailed technical nature suggests this document would be part of an RFP or grant for manufacturing, procurement, or related aerospace engineering projects.

This document, FLL-HPROJ-0094, details the specifications for an "UPPER ELEVON IN/OUTBOARD C CHANNEL" component for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. The component, identified as "1JYR2-FLL-HPROJ-0094-101," is made from C Channel C3x4.1 A36 steel stock per ASTM A36/A36M. It requires a specific finish: one coat of MIL-PRF-23377 epoxy primer and two coats of MIL-PRF-85285 polyurethane, color 15092 (OSHA Safety Blue), with holes masked prior to painting. Human-readable identification marking, including the part number and latest revision, must be applied per MIL-STD-130 using permanent ink. The document includes detailed dimensions, tolerances, and engineering approvals, with a revision history indicating its initial release. It also contains an EAR99/NLR notice, clarifying that the information is technical but not subject to ITAR or EAR technology definitions, though export or re-export contrary to embargo provisions is prohibited. This file is a technical drawing outlining the manufacturing and finishing requirements for a specific aerospace component.

This government file details the design and specifications for the "UPPER ELEVON IN/OUTBOARD LOCKS" for the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center. The document outlines the components, materials, and assembly instructions for both inboard and outboard lock sections. Key components include A36 steel sheet for U-sections and stiffener plates, along with self-locking nutplates, solid rivets, hex bolts, and washers. The file specifies material per ASTM A36/A36M and fasteners per MS21076L4N, MS20426AD3-4, 92620A565, and 92141A029. Finishing requirements include a primer/top coat system per MIL-DTL-18264, with epoxy primer (MIL-PRF-23377) and polyurethane topcoat (MIL-PRF-85285) in OSHA Safety Blue. Identification marking per MIL-STD-130 is also required. Detailed drawings provide dimensions and tolerances for each part, with specific instructions for rivet installation (NASM47196) and bolt tightening torque (25-35 IN-LB). The document also includes an EAR99/NLR notice, indicating that the information is technical but not restricted by ITAR or EAR, though export prohibitions apply.

This document, FLL-HPROJ-0092, from the National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center, details the design specifications for the "Upper Elevon In/Outboard LS" components, specifically the -101 Upper Elevon Inboard Angle Detail and the -103 Upper Elevon Outboard Angle Detail. The file includes engineering drawings, dimensions in inches with specified tolerances, material requirements (A36 steel stock per ASTM A36/A36M), and finishing instructions. The finishing involves a primer/top coat system conforming to MIL-DTL-18264, with specific epoxy primer (MIL-PRF-23377) and polyurethane topcoats (MIL-PRF-85285, color 15092, OSHA Safety Blue per SAE AMS-STD-595). It also specifies human-readable identification marking per MIL-STD-130. The document is marked as EAR99/NLR, indicating it is not subject to ITAR or EAR technology definitions, but still subject to export control regulations regarding embargoed countries. Approvals and revision history are also provided.

NASA's Request for Quotation (RFQ) 80NSSC26922577Q seeks proposals for the fabrication and delivery of Upper Elevon Heater Carriage components for the NASA Armstrong Flight Research Center. The project, set aside for small businesses, requires vendors to fabricate test hardware according to provided design drawings within 12 weeks of contract award. Proposals must include a manufacturing process plan and a quality plan. Evaluation will be based on a "best value" approach considering the lowest price, fabrication duration, past performance (with three references), and technical acceptability. Quotes are due by January 21, 2026, 4:00 p.m. CT, and all questions must be submitted in writing by January 19, 2026, 12:00 p.m. CT. Offerors must be registered with www.sam.gov and provide their CAGE Code/UEI, ARO Delivery Time, and FOB Destination. The solicitation incorporates various Federal Acquisition Regulation (FAR) and NASA FAR Supplement (NFS) provisions and clauses, including those related to representations and certifications concerning small business status, telecommunications equipment, and other compliance requirements.

NASA Armstrong Flight Research Center (AFRC) is seeking a contractor to fabricate and deliver components for an Upper Elevon Heater Carriage. This Statement of Work details the fabrication of test hardware according to NASA AFRC's design drawings. The contractor is expected to complete fabrication and delivery within 12 weeks of contract award, with earlier delivery being desirable. Deliverables are to be shipped to NASA AFRC in Edwards, CA, with one week's advance notice for logistics coordination. Proposals must include a manufacturing process plan and a quality plan for dimensional tolerances. NASA AFRC will conduct a "best value" evaluation based on lowest price, fabrication duration, past performance (three references from the last three years), and technical acceptability. The contractor must provide status updates every three weeks via email and document any requested changes to the provided drawings. NASA AFRC will supply numerous drawings for components such as Elevon Dolly, Water Manifold Bracket, Axis Features, Reflector Frames, and various other structural and linkage parts.