What are the responsibilities and job description for the Liquid Rocket Propulsion Research Engineer position at Air Force Research Laboratory?
Job Overview
This job announcement will be accepting candidate submissions until 12 May 2026.
The AFRL Rocket Science and Technology Division (AFRL/RQR), Aerospace Systems Directorate, seeks to fill a mid-level position at the DR-02 or DR-03 levels (depending on qualifications and experience) as Liquid Rocket Propulsion Research Engineer . The position is located at the AFRL Rocket Laboratory at Edwards AFB, CA.
For more than 60 years, the AFRL Rocket Laboratory at Edwards AFB has contributed to several technology developments in rocket engines, including those of Saturn, Titan, Space Shuttle, and all major intercontinental ballistic missiles and current space launchers. Today, the site continues to enable technology leaps in hypersonics, solid rocket boosters, in-space propulsion, and liquid rockets for defense and commercial space in support for the Air & Space Forces.
We are searching for a high-performing, highly-motivated individual with a strong background in advanced liquid rocket engine technologies .
Position duties include, but are not limited to:
Yes, this position is eligible for situational telework; as determined by agency policy
Eligible for a Referral Bonus?
Yes
Required Qualifications
Must be able to travel
Requsition Number 49706
Series
0830
0861
This job announcement will be accepting candidate submissions until 12 May 2026.
The AFRL Rocket Science and Technology Division (AFRL/RQR), Aerospace Systems Directorate, seeks to fill a mid-level position at the DR-02 or DR-03 levels (depending on qualifications and experience) as Liquid Rocket Propulsion Research Engineer . The position is located at the AFRL Rocket Laboratory at Edwards AFB, CA.
For more than 60 years, the AFRL Rocket Laboratory at Edwards AFB has contributed to several technology developments in rocket engines, including those of Saturn, Titan, Space Shuttle, and all major intercontinental ballistic missiles and current space launchers. Today, the site continues to enable technology leaps in hypersonics, solid rocket boosters, in-space propulsion, and liquid rockets for defense and commercial space in support for the Air & Space Forces.
We are searching for a high-performing, highly-motivated individual with a strong background in advanced liquid rocket engine technologies .
Position duties include, but are not limited to:
- Oversees technical programs to address Department of War’s technical needs in tactically responsive space, orbital warfare, affordable mass, and national missile defense.
- Provides technical, scientific, programmatic and strategic advice on aspects related to liquid rocket engines and their integration into air & space vehicles.
- Envisions, formulates, and tests new capability concepts for liquid rocket propulsion, including new propellants, materials, controllers, powerheads, propellant management systems, cooling systems, and thermodynamic cycles.
- Executes technical programs and coordinates major reviews and milestones.
- Interfaces with customers and partners testing in our facilities.
- Interfaces with partners in industry, academia, and other government agencies.
Yes, this position is eligible for situational telework; as determined by agency policy
Eligible for a Referral Bonus?
Yes
Required Qualifications
- US Citizenship.
- Ability to obtain and maintain a Secret security clearance.
- B.Sc. or M.Sc. in Aerospace Engineering, Mechanical Engineering, or Aeronautical Engineering.
- This position is an Acquisition Professional Development Program (APDP) position requiring level 1-Foundational, Non-Critical certification in Engineering & Technical Management. The selectee will have 24-months to meet APDP requirements or a waiver must be obtained. Government applicants for this position must list any acquisition certifications and status as an acquisition corps member in their resume.
- Strong background in liquid rocket propulsion.
- Experience in research, analysis, design, development, and test of liquid rocket engines or their subcomponents.
- Experience in operating rocket experimental facilities.
- Experience with engineering aspects of integrating liquid rocket engines into air or space vehicles, including but not limited to: Air & space flight mechanics, mass properties, powerheads, thrust vector control, throttling, and thermal control.
- Experience in writing technical manuscripts and giving briefings or conference presentations to broad audiences.
- Familiarity with explosives safety.
- Familiarity with detonation-based (RDRE) liquid rocket engines.
- Excellent communication skills to interface with scientists, engineers, and program managers.
Must be able to travel
Requsition Number 49706
Series
0830
0861