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Aerospace & Defense Engineering Search

Hire Propulsion Engineers

Hire Propulsion Engineers who own liquid and solid rocket propulsion and in-space propulsion — engine cycle analysis, turbomachinery, injectors and combustion, feed and pressurization systems, hot-fire test support, solid rocket motor design and thruster development — for launch vehicle, spacecraft, hypersonics and defense propulsion product teams. Verified with the chief engineers and test conductors who reviewed their hardware, not the resume.

Propulsion Engineer - iRecruit.coExample profile
Mei A.
Vetted Specialists
MEP & Engineering
Propulsion Engineer
MSAE · Liquid Engine Development · ITAR U.S. Person
Sectors
Space & defense
Launch vehicles, in-space propulsion, hypersonics, tactical and strategic solid motors, defense propulsion primes
Role scope
Engineering search
Retained and direct-hire searches, Engineer II through Principal and Chief Engineer, for space, defense-tech and advanced-manufacturing product teams
Geography
US-wide
Industrial, defense and mission-critical network
Placement warranty
Replacement guarantee
Every model, every placement
How It Works

Hire Propulsion Engineers in 3 steps

A structured process for the hire whose analysis decides whether the engine closes — where a Propulsion Engineer who has only run a cycle deck in school undersizes the turbopump margin, misses a chug instability on the injector, and the program learns it on the stand at $2M per hot fire instead of in the design review.

Step 01

Talk to our team

30-minute call. Align on propulsion type (liquid engine, solid motor, hybrid, monoprop or bipropellant thruster, electric propulsion), engine cycle and propellants (gas generator, staged combustion, expander, pressure-fed; LOX/methane, LOX/RP-1, LOX/hydrogen, hypergols, green monoprops), subsystem ownership (turbomachinery, injector and chamber, feed and pressurization, valves, igniters, nozzles, grain design), program phase (concept, development, qualification, production), test-support expectations, ITAR and clearance, reporting line, and start date.

Step 02

Review hand-selected talent

Within 2 weeks we introduce 3–5 Propulsion Engineers with verified design ownership on comparable cycles and propellants — hardware that went to hot fire or static fire, not coursework or analysis-only resumes restyled. References from chief engineers, test conductors and responsible engineers included.

Step 03

Hire with confidence

Every placement carries a replacement guarantee. If the hire fails within the warranty window, we run a no-fee replacement search.

Why iRecruit.co for Propulsion Engineer Hires

What makes our Propulsion Engineer shortlist different

A Propulsion Engineer on a launch or spacecraft program is judged by engines that close on performance and mass, hardware that survives its first hot fire, and test anomalies resolved before the next campaign. Design ownership that reached the stand, cycle-analysis depth and combustion-stability scars separate an engineer who delivers propulsion from one who models it.

01

Design ownership verified through hot fire

Every Propulsion Engineer has reference-verified responsibility for a component or subsystem that fired — injector, chamber, turbopump, feed system, valve, igniter, solid motor grain or thruster — from requirements through CDR, build and test. We confirm what they owned, what failed and what they changed with the chief engineer or responsible engineer, not the program list.

02

Cycle analysis and combustion fluency

Engine cycle balance and power-balance modeling (RPA, NPSS, in-house decks), CEA and equilibrium chemistry, injector element design and mixing, combustion stability (chug, buzz, high-frequency modes) and acoustic damping, regenerative and film cooling, nozzle contour and performance prediction, turbopump hydrodynamics, cavitation and rotordynamics, and solid motor ballistics and grain design. Matched to your cycle and propellants, not a generic mechanical engineer.

03

Feed systems, test support and anomaly resolution

Verified ownership of feed and pressurization system sizing, tank and line pressure drops, water-hammer and priming transients, valve and regulator specification, P&ID authorship, oxygen-compatibility and material selection, hot-fire test planning and redline definition, post-test data review, and root-cause investigation of hardware anomalies with corrective design changes that reached the next build.

Meet Vetted Propulsion Engineers

The caliber of Propulsion Engineer you’ll interview

Every candidate is credential-verified, reference-checked, and matched to your propulsion type, cycle and program phase. Anonymized examples below reflect real placement profiles.

Vetted SpecialistsFemale Propulsion Engineer - launch vehicle programExample profile

Priya K.

Propulsion Engineer, Liquid Engine Injector and Combustion
  • Responsible engineer for the main injector of a 200 klbf-class LOX/methane gas-generator engine — element design, manifold hydraulics and face cooling through CDR, 3 build iterations and 85 hot fires
  • Resolved a 1,100 Hz chug instability at low-throttle by re-tuning injector pressure drop and adding acoustic cavities, verified stable across 40–110% throttle in 12 dedicated stability tests
  • Owned CEA and in-house cycle balance updates that closed the engine on Isp and mass targets after a 6% turbine-inlet-temperature reduction driven by materials
Injector designCombustion stabilityCycle analysis
Vetted SpecialistsMale Propulsion Engineer - solid motor plantExample profile

Darnell W.

Senior Propulsion Engineer, Solid Rocket Motors
  • Designed grain geometry and ballistics for a tactical boost motor to a 15-second thrust-time trace within 3% of prediction on first static fire, including insulation and liner thickness margins
  • Owned nozzle and igniter design for a two-pulse strategic motor through qualification — 14 static fires, thermal-structural analysis of the throat and exit cone, MIL-STD-1901 igniter safety review
  • Led root cause on a case-bond anomaly found in CT inspection, changing the cure profile and liner process and retiring the finding across 3 motor lots
Grain design and ballisticsNozzle and igniterQualification test
Vetted SpecialistsFemale Propulsion Engineer - spacecraft manufacturerExample profile

Omar Z.

Lead Propulsion Engineer, In-Space Propulsion and Feed Systems
  • Owned the bipropellant propulsion subsystem for a GEO satellite bus — 22 N and 450 N thrusters, feed and pressurization schematics, valve and regulator specs, 8 pressure-drop and priming-transient models delivered to PDR and CDR
  • Qualified a green-monopropellant thruster from engineering model through 60,000-second life test, owning catalyst bed thermal design and the hot-fire test plan and redlines
  • Cut propellant-loading and leak-check time 30% by redesigning fill-and-drain valve layout and P&ID for a 6-satellite-per-month production line
Feed and pressurizationThruster qualificationSpacecraft propulsion
Propulsion Engineer Specializations

Match the Propulsion Engineer specialty to your engine and program

“Propulsion Engineer” ranges from a cycle analyst who closes the engine on paper to a turbomachinery designer to a feed-systems owner to a solid-motor ballistician, and the right hire depends on which subsystem is holding your program. Below are the specializations we recruit for:

Not sure which Propulsion Engineer specialty fits?

We’ll help you scope the role on the call — propulsion type and cycle, propellants, subsystem ownership, program phase, test-support expectations, and clearance requirements.

Hire Propulsion Engineers →
Vetting Criteria

What we verify on every Propulsion Engineer candidate

Propulsion Engineer hires live and die on engines that close, hardware that survives hot fire, and anomalies resolved before the next campaign. Below is what every candidate has documented before you meet them:

Design ownership through hot fire

Reference-verified responsible-engineer history on a propulsion component or subsystem that went to hot fire or static fire — requirements, design reviews, build support, test results and design changes — confirmed by the chief engineer or responsible engineer.

Cycle analysis and combustion depth

Verified working fluency in engine cycle balance, CEA and equilibrium chemistry, injector and chamber design, combustion stability assessment, cooling analysis and nozzle performance prediction, or solid motor ballistics and grain design, matched to your propulsion type.

Feed systems and fluid components

Verified ownership of feed and pressurization sizing, transient analysis, valve and regulator specification, P&ID authorship, oxygen and propellant material compatibility, and cleanliness and contamination control for flight fluid systems.

Test support and anomaly resolution

Verified history writing test plans and redlines, reviewing hot-fire data, running root-cause investigations on hardware anomalies, and carrying corrective design changes into the next build under configuration control.

Credentials verified

ABET aerospace or mechanical engineering degree, graduate degree where held, analysis tool proficiency (RPA, NPSS, CEA, Ansys, NX or Creo, MATLAB or Python), US-person status where ITAR applies, and active clearance where the program requires it — all checked.

Compensation alignment

Engineer II, Senior, Staff and Principal comp bands aligned before finalists are introduced, including test-campaign travel expectations, remote test-site time, clearance premium, relocation, and equity where offered.

FAQ

Hiring a Propulsion Engineer: frequently asked questions

How long does it take to hire a Propulsion Engineer?

Time to shortlist is typically 2 weeks from scoping call. Total time to placement (shortlist through offer acceptance) is typically 3–5 weeks. Seats requiring staged-combustion or hydrogen turbomachinery depth, solid motor qualification history, an active clearance, or relocation can run a week or two longer, and Principal and Chief Engineer searches are typically run as retained engagements with a longer calendar.

What does a Propulsion Engineer cost in 2026?

Most US Propulsion Engineers at launch, spacecraft and defense propulsion companies land between $110K and $150K base at the Engineer II-to-Senior level depending on metro and subsystem. Staff and Principal Propulsion Engineers with responsible-engineer history on flight engines, turbomachinery or qualified solid motors typically run $150K–$210K, with chief engineers and propulsion leads above that. Launch and defense programs commonly add clearance premiums and equity. These are market bands; we confirm live market bands during scoping. See our propulsion engineer salary guide for a fuller breakdown.

How is a Propulsion Engineer different from a Propulsion Test Engineer?

A Propulsion Test Engineer owns the stand: fluid systems, instrumentation, sequences, abort logic and hazardous operations. The Propulsion Engineer owns the hardware on the stand and the analysis behind it: cycle, injector, turbopump, feed system, motor grain. The two meet at test readiness reviews and post-test data review, and on small teams one person may carry both, but the design seat and the stand seat are different searches.

How is a Propulsion Engineer different from a Mechanical Design or Thermal Engineer?

A Mechanical Design Engineer owns structures, mechanisms and CAD across the vehicle; a Thermal Engineer owns thermal analysis and protection. The Propulsion Engineer owns the engine or motor as a system and the combustion, fluid and turbomachinery physics inside it, and pulls design and thermal support in. A Structural Analysis Engineer typically clears the chamber, case and turbopump housings the propulsion engineer specifies.

How is a Propulsion Engineer different from a Systems or GNC Engineer?

A Systems Engineer owns requirements, interfaces and verification across the vehicle; a GNC Engineer owns how the vehicle uses thrust vector control and throttle. The Propulsion Engineer delivers the thrust, Isp, throttle range and gimbal authority those two depend on. All three sit in the same trade studies; the propulsion seat owns the engine-level answers.

Do you require a graduate degree or a clearance?

It depends on the seat. Many strong liquid-engine and turbomachinery engineers hold an MS or PhD, and some cycle and combustion seats call for it, but we verify design ownership that reached hot fire through references rather than screening on degree. Clearances depend on the program: we confirm the requirement during scoping, verify US-person status where ITAR applies, and verify active clearance directly rather than taking a resume claim.

Do you offer a placement guarantee?

Yes. Every Propulsion Engineer placement carries a replacement guarantee. Guarantee terms are confirmed in writing at engagement start.

Can you build a full propulsion team?

Yes. Multi-hire builds (a chief engineer plus cycle, turbomachinery, combustion devices, feed systems and test-support engineers for a new engine program, or a solid motor design group ahead of a production ramp) route through embedded recruiting or RPO. Single retained searches run through aerospace and defense engineering search, and confidential chief engineer and VP Propulsion seats route through executive search.

Ready to hire

Talk to an engineering search recruiter

30-minute scoping conversation. We’ll review the Propulsion Engineer role you need — propulsion type and cycle, propellants, subsystem ownership, program phase, test-support and clearance requirements — then recommend the right hire path and start sourcing.

Prefer to talk it through?
Book a 30-minute intro call and leave with pricing, timelines, and next steps.
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