Tyler Lamb Email & Phone Number

Sunnyvale, California, United States

• Manage mechanical engineering team of 16 direct reports responsible for development and delivery of Multiple All up Round Canister (MAC), Advanced Payload Module (APM), Component Test Fixtures, and System Test Hardware.
• Development of employees through training and placement into strategic assignment to maintain and develop engineering team's critical skills
• Oversight of hardware and project execution for multiple component test fixture, system test, MAC, and APM hardware items
• Responsible for development of process and tool to improve CPS program efficiency and execution
• Responsible for supporting staffing of Launcher programs to ensure resource and talent demands are met to enable program execution of work scope
• Oversight and approval authority for proposing engineering labor basis of estimates for Launcher program proposal efforts

Sunnyvale, California, United States

• P21 Program Alternate Test Stand (ATS) Integration Engineering Lead
• Design authority for labor budget of $322K and for $380K of material
• Developed proposal BOEs for 9621 labor hours of design effort and $380K material in rapid 1 month proposal effort with very few internal and customer findings
• Completed successful conceptual design review of ATS Adaptor hardware design in 6 weeks
• Met program schedule for successful completion of internal PDR in 6 months for all hardware kits, and internal FDR in 10 months, including the closeout of 16 drawing TTRs, and release 30 drawings, 2 test plans, 14.
• Successfully led team in support of all hardware procurement and integration at offsite vendor facility to meet aggressive schedule for TD7A.1 test

Azusa, CA

• Joint Polar Satellite System (JPSS) 2 Advanced Technology Microwave Sounder (ATMS) Program – Hosted Payload
• Design authority for developing Instrument Level Integration and Test (II&T) CDR content and presenting to NASA customer at Program Delta CDR, and for authoring II&T Procedure the new JPSS-2 ATMS configuration
• Led requirements definition, planning, and redesign of Receiver Shelf Integration Fixtures to improve alignment effectiveness, repeatability, and safety from requirements definition through final drawing release
• Completed initial trade study and requirements definition of JPSS2 cable forming fixture manufacturing improvement effort in support of new JPSS-2 ATMS configurationModular Space Vehicle (MSV) Task Order 3 (TO3).
• Responsible for Modular Space Vehicle-Task Order 3 (MSV-TO3) Data Collector Assembly (DCA) ICD.
• MSV-TO3 Launch Lock Mechanism Design Lead. Took design from PDR level design maturity to 100% drawing release on schedule for program CDR. Responsible for checking of all launch lock drawings and completing all flight.

El Segundo, California

• Design Lead – ICDs, Master Datums, Major Installations, and Final Assembly
• Probe and Receptacle Aerial Refueling program Subject Mater Expert. Developed configuration layout and structural design of Aerial Refueling structure and retrofit.
• Played integral role in program transition from CATIA/MEDs to NX/CPLM by creating T-X program NX Quick Start Guide and holding productivity training session for NX, VisPro, and CPLM
• Led T-X fuel sealing weight and cost trade study to down select overcoat fuel sealing process that eliminated 650 fasteners and created and estimated lifetime program savings of $1 million
• Coordinated with BAE Systems engineers on program CAD modeling tools selection, ICD and Master Datum File development, and engineering work share at major mates

El Segundo, CA

• Supported successful release of SES-9 satellite antenna structural design
• Provided design support for review and checking of structural definition of parts in release cycle
• Led manufacturing and assembly of the SES-9 antenna structure and spacecraft integration
• Resolved antenna integration anomalies during assembly process and drove to closure through customer collaboration
• Led supplier source selection and supplier collaboration effort in cost savings initiative to standardize common parts between multiple programs

St Louis, MO

• Demonstrated a >50% hrs/lb reduction in design and assembly of structure in an innovative, production-like environment
• Responsible for design of thermoplastic, titanium, and aluminum substructure
• Led pre-Conceptual Layout (PCLO) phase trade studies, and created program checkmate profile
• Supported structural design through PCLO, CLO, assembly layout (ALO), and build to print (BTP) program phases
• Responsible for peer review of primary aircraft structure through BTP release phase

St Charles, MO

• 2000lb Joint Direct Attack Munitions Extended Range (JDAM-ER) – Extended Range Wingkit Design
• Completed an asymmetrical wing lofting and fitment to meet program aircraft integration requirements
• Led asymmetrical wing deployment mechanism trade study and design, complex deployment linkage analysis, and wing deployment motion simulation to meet program PDR requirements500lb JDAM-ER – Productionization of.
• Teamed with Boeing Aerospace Australia to conduct an initial design assessment and configuration study to reduce product cost and complexity, and enhance product reliability and capabilities
• Completed redesign of major structural wing kit components to reduce part count by 30%
• Interfaced with US Navy and Air Force customers to define future logistics integration requirements500lb Enhanced JDAM-ER – Structural design of propulsion section to extend range of 500lb JDAM-ER

Ms, Mechcanical Engineering

B.E., Mechanical Engineering

Activities and Societies: University Student Launch Initiative, Vanderbilt Aerospace Club, Sigma Phi Epsilon