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Mechanisms Engineer

Job in Midland, Midland County, Texas, 79701, USA
Listing for: ZP Group
Per diem position
Listed on 2026-06-05
Job specializations:
  • Engineering
    Mechanical Engineer, Systems Engineer, Manufacturing Engineer
Salary/Wage Range or Industry Benchmark: 85 USD Hourly USD 85.00 HOUR
Job Description & How to Apply Below
Piper Companies is currently looking for a Mechanisms Engineer in Midland, TX to work for a rapidly growing satellite production company. This role requires the candidate to report onsite and offers significant relocation and benefits packages.

Responsibilities for the Mechanisms Engineer:

* Assemble, integrate, and test spacecraft mechanisms including hinges, yokes, actuators, HDRMs, and deployable booms/arms with thousands of moving parts per satellite.

* Develop and operate ground support equipment for vibration, shock, and thermal vacuum testing of deployment hardware.

* Perform tolerance stack-up analysis and ensure alignment in moving assemblies for reliable deployment.

* Analyze test data and determine pass/fail criteria, supporting spacecraft integration and launch operations.

* Troubleshoot anomalies and perform root-cause analysis on deployment systems; contribute to design improvements for mechanisms that fail to deploy cleanly.

* Collaborate cross-functionally with engineers and technicians to ensure mechanism performance from design through mission deployment.

* Calculate torque margins and hinge preload requirements for deployment actuators and separation systems.

Qualifications for the Mechanisms Engineer:

* 0-4 years of hands-on experience in aerospace mechanisms, deployment systems, or precision mechanical assemblies (structures-only experience will not suffice).

* Proficiency in mechanical assembly, testing, and integration of space hardware, including deployable systems.

* Experience with CAD tools (Solid Works, Creo) and test equipment (oscilloscopes, thermal chambers).

* Bachelor's degree in Mechanical, Electrical, Manufacturing, or Industrial Engineering (or equivalent experience).

* Strong understanding of beam loading, bending moments, torque margins, and tolerance stack-ups in moving assemblies.

* Excellent problem-solving and analytical skills; ability to lead failure investigations.

* Flexibility for occasional weekend and early morning work (e.g., 4 AM deployments).

Compensation for the Mechanisms Engineer:

* Salary Range: $85,+ (depending on experience)

* Comprehensive benefit package;
Cigna Medical, Cigna Dental, Vision, 401k w/ ADP, PTO, paid holidays, sick Leave as required by law

This job opens for applications on 4/6/26. Applications for this job will be accepted for at least 30 days from the posting date

#LI-BM2

#LI-ONSITE

mechanism AIT, precision assembly, cleanroom integration, contamination control, mechanical tolerance stack-up, kinematic chain, degree of freedom management, load path definition, structural load transfer, deployment kinematics, deployment dynamics, hinge line alignment, hinge preload, over-center mechanism, hard stop, soft stop, deploy latch, hold-down release mechanism, HDRM, HDRM pin puller, frangibolt, non-explosive actuator, NEA, shape memory alloy actuator, SMA actuator, motor-driven actuator, stepper motor, brushless DC motor, torque motor, gear train, planetary gearbox, harmonic drive, cycloidal drive, spur gear, backlash control, preload springs, Belleville washers, torsion spring, constant force spring, flexural pivot, flexure hinge, compliant mechanism, yoke assembly, clevis joint, spherical bearing, duplex bearing, angular contact bearing, bearing preload, dry lubricant, MoS₂ coating, sputtered lubricant, solid lubrication, grease compatibility, vacuum-rated lubricant, tribology, wear-in testing, life-cycle testing, deployment life testing, microgravity deployment analysis, gravity offload system, counterbalance rig, air-bearing table, gravity compensation fixture, test-as-you-fly philosophy, flight-like configuration, protoflight approach, qualification model, flight model, engineering model, pathfinder unit, breadboard unit, mechanism-level qualification, subsystem-level qualification, system-level test, acceptance testing, workmanship verification, torque margin, torque budget, torque scatter, torque signature, motor current profile, deployment time margin, latch confirmation switch, microswitch, reed switch, Hall effect sensor, position encoder, resolver, potentiometer, end-of-travel sensing, redundant sensing, single-fault tolerance, fail-safe design, fail-operational design, inhibit lines, arm/disarm plug, safing pin, remove-before-flight pin, RBF pin, ground safety constraints, ground support equipment, GSE, electrical ground support equipment, EGSE, mechanical ground support equipment, MGSE, deployment restraint, launch lock, launch vibration restraint, preload retention, random vibration testing, sine vibration testing, shock testing, pyroshock testing, modal survey, resonance avoidance, dynamic coupling, modal margin, stiffness margin, thermal distortion, thermal vacuum testing, thermal cycling, thermo-mechanical analysis, coefficient of thermal expansion mismatch, CTE mismatch, cold deployment, hot deployment, worst-case deployment, deployment repeatability, deployment symmetry, synchronization mechanism, timing gear, cross-shaft, cable-driven…
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