Senior System Architect – Optical Communications
The role is part of the In-Space Systems business unit focused on space infrastructure and on-orbit mobility.
As the Senior System Architect for our next-generation optical communications program, you will define the end-to-end technical vision for a system designed to set new standards in space-based connectivity. You will own the architecture for an optical communications system, translating mission objectives into a resilient, high-performance system ready for the space environment.
- Define the end-to-end mission architecture, including wavelength selection, link geometry, autonomy, redundancy strategies, and initial SWaP–T allocations.
- Drive system-level trades for the terminal's aperture, balancing link margin, pointing accuracy, throughput, structural stiffness, and thermal management.
- Flow down performance budgets to all subsystems (optics, PAT, modem, electronics) with rigorous ICDs and calibration strategies.
- Integrate STOP analysis into system budgets and define acceptance criteria for hardware verification and vendor SOWs.
- Define PAT concept of operations and control architecture, model and simulate key performance parameters.
- Develop validation strategy for PAT algorithms from simulation to advanced mirror materials.
- Define modem and electronics development plan, ensuring deterministic latency, fault tolerance, and radiation resilience.
- Author and manage core systems engineering documents, identify technical risks, lead architecture reviews, and serve as primary technical authority.
- Lead rapid prototyping efforts, create feedback loops, and coordinate cross‑functional teams.
Travel: Up to 15 % to supplier facilities, test sites, and Blue Origin locations.
Relocation assistance may be available.
Minimum Qualifications
- Bachelor’s degree in Systems Engineering, Electrical Engineering, Optical Engineering, or related field; 7+ years relevant experience (M.S./Ph.D. preferred).
- End-to-end system design experience in high-throughput optical communications (free-space or fiber).
- Mastery of optical link budget analysis, including pointing loss, atmospheric/diffraction effects, jitter coupling, and capture probability.
- Experience designing and analyzing control systems (filters, scan strategies, beacon processing).
- Familiarity with FPGA/ASIC architectures, SerDes interfaces, deterministic memory/DMA, high-speed data paths.
- Proven systems engineering rigor in authoring ICDs, decomposing requirements, and developing verification plans.
- Experience with radiation-hardened design principles, SEU mitigation, and radiation-tolerant components.
- Must be a U.S. citizen, permanent resident, or lawfully admitted U.S. resident.
Preferred Qualifications
- Experience with optical systems, straylight, and contamination control.
- Familiarity with space hardware development lifecycles and standards (DO-254, ECSS).
- Experience designing built-in-test, telemetry, and fault management systems.
- Hands-on hardware-in-the-loop validation.
- Knowledge of coherent and incoherent detection methods and advanced modulation formats.
Senior Opto‑Mechanical Engineer
The role is part of the In-Space Systems business unit focused on space infrastructure and on-orbit mobility.
As a Senior Opto-Mechanical Engineer, you will lead the mechanical design for the optical heart of a communications terminal. You will own the physical system from concept and material selection through final assembly and validation.
- Lead mechanical design of the telescope structure, incorporating precision alignment features, kinematic mounts, and athermal principles.
- Develop comprehensive tolerance budgets for WFE and alignment stability, informed by STOP analysis.
- Engineer solutions for straylight and ghost suppression, including baffle design and scatter control.
- Author and manage contamination control plans and cleanliness procedures.
- Ensure designs are optimized for manufacturability, assembly, and alignment (DFMA), defining necessary tooling and GSE.
- Provide technical mentorship to junior engineers.
- Lead development path and trade studies for mirror materials, evaluating CTE stability, stiffness, polishability, and thermal performance.
- Draft detailed SOWs for vendors and manage relationships, ensuring compliance.
- Collaborate with STOP analyst to define stiffness targets and integrate thermal control hardware.
- Lead cross-functional technical reviews to ensure integrated system performance.
- Plan and oversee environmental qualification tests, including thermal cycling, dimensional stability, and vibration testing.
- Provide hands-on support for optical alignment, integration, and metrology activities in the lab.
- Refine designs based on straylight test data and validate contamination control procedures.
- Develop and document lessons learned to improve future designs.
Travel: 10–15 % to vendor visits, design reviews, and test campaigns.
Relocation assistance may be available.
Minimum Qualifications
- Bachelor’s degree in Mechanical Engineering, Aerospace Engineering, or related field; 10+ years relevant experience (M.S./Ph.D. preferred).
- Demonstrated experience designing telescopes or similar precision optical instruments for space or aerospace applications.
- Proven expertise in straylight analysis, contamination control, baffle design, and coating selection.
- Hands-on experience with advanced mirror materials and their fabrication, polishing, and testing methods.
- Experience integrating mechanical designs with structural, thermal, and optical performance analyses.
- Proficiency in a major CAD package (e.g., PTC Creo, Siemens NX).
- Experience leading technical teams and mentoring junior engineers.
- Track record of successful delivery of complex opto-mechanical systems for demanding applications.
- Must be a U.S. citizen, permanent resident, or lawfully admitted U.S. resident.
Preferred Qualifications
- Direct experience using STOP analysis to drive mechanical design decisions.
- Experience with space environmental testing (thermal cycling, vibration, TVAC) and test-model correlation.
- Design or integration experience with precision pointing mechanisms or gimbals for space.
- Knowledge of athermalization techniques for optical systems.
- Experience developing and executing optical alignment procedures using interferometry and other metrology tools.
- Previous experience with optical communications systems or laser-based instruments.
- Experience with systems engineering practices and requirements flow-down.
- Publication record or patents in relevant technical areas.
Structural & Thermal Engineer
The role is part of the In-Space Systems business unit focused on space infrastructure and on-orbit mobility.
As a Structural & Thermal Engineer focused on STOP analysis, you will serve as the analytical backbone, ensuring our optical systems achieve peak performance from launch through on-orbit operations.
- Perform coupled STOP analysis, integrating structural, thermal, and optical design models.
- Derive, allocate, and close optical performance budgets (e.g., alignment, WFE) with optical and mechanical engineers.
- Bound system sensitivities to environmental and structural inputs and propose design mitigations.
- Build and maintain high-fidelity FEA models to analyze modal response, random vibration, shock, and quasi-static loads.
- Analyze and mitigate gravity release and mount preloads on optical alignment and surface figure.
- Quantify structural stiffness and jitter transfer functions to ensure fine-pointing stability.
- Develop detailed thermal models to simulate radiation, conduction, and active thermal control systems.
- Manage thermal dissipation and ensure optical stability across operational and survival modes.
- Translate thermoelastic distortions into quantified impacts on optical performance.
- Define a comprehensive model validation plan, including instrumentation requirements for environmental testing.
- Correlate analytical models with TVAC and vibration test data, iterating to improve accuracy.
- Develop and present evidence packages for system feasibility, including model pedigree, uncertainty analysis, and sensitivity studies.
Minimum Qualifications
- Bachelor’s degree in Mechanical Engineering, Aerospace Engineering, or related field; 7+ years relevant experience (M.S./Ph.D. preferred).
- Expertise in FEA for precision space structures, with experience in modal/dynamic analysis, random vibration, and thermoelastic distortion.
- Deep understanding of passive and active thermal control systems for space applications.
- Strong skills in uncertainty quantification, probabilistic analysis, Monte Carlo methods, and sensitivity studies.
- Proficiency with relevant analysis software (FEA: Nastran, Ansys, or Abaqus; Thermal: Thermal Desktop, SINDA/FLUINT, or similar).
- Must be a U.S. citizen, permanent resident, or lawfully admitted U.S. resident.
Preferred Qualifications
- Mastery of coupling structural/thermal models with optical design tools (Zemax, Code V, or similar).
- Experience with telescopes, complex optics, or gimbaled systems.
- Background in designing low-jitter structures, including isolation systems or damping.
- Experience with test correlation, including pre-test analysis and post-test model updates for TVAC or vibration campaigns.
- Proficiency in a scripting language (Python, MATLAB) for data analysis, process automation, and parametric studies.