CourseAerospace, UAM, Drones & Space Applications open

Orbital Transfer Course

Online course of 300 hours in orbital transfers, structured in 6 modules covering impulsive manoeuvres, coplanar transfers, Lambert's problem and general transfers, low-thrust transfers and trajectory optimisation, with an assigned technical tutor.

Duration3 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute certificate

Orbital Transfer Course — studying from the United States

The United States leads global aerospace, anchored by clusters in Seattle, Wichita, Hartford, Huntsville and the Houston area. Major employers such as Boeing, Lockheed Martin, RTX and GE Aerospace drive demand for engineers in airframes, propulsion, avionics and systems integration. Urban air mobility and commercial drone operations are expanding quickly, creating new roles in eVTOL design, airspace integration and UAS operations. Civil and military programs both rely heavily on certified design, testing and airworthiness processes, making this a strong field for engineers seeking complex, high-impact work.

Fees for the United States: 720 US$ (US Dollars), with instalments and employer sponsorship available.

Relevant bodies in the United States

  • Federal Aviation Administration (FAA)
  • National Aeronautics and Space Administration (NASA)
  • SAE International
  • RTCA, Inc.

Typical roles

  • Aerospace Engineer
  • Flight Test Engineer
  • Propulsion Systems Engineer
  • UAS Systems Engineer

Questions from the United States

Can I study from any state?

Yes. Programmes are 100% online, so you can study from anywhere in the United States with a reliable internet connection.

Is the programme taught in English?

Yes. All programmes are taught in English, with technical materials and assessments delivered in that language.

Virtual lab · try it before you enrol

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Learning outcomes

What you will be able to do

01

Calculate impulsive manoeuvres and their Δv budget.

02

Compare Hohmann and bi-elliptic transfers.

03

Solve Lambert's problem for general transfers.

04

Design interplanetary transfers using patched conics.

05

Analyse continuous low-thrust transfers.

06

Apply trajectory optimisation methods.

07

Prepare a manoeuvre plan for a real mission.

Profile

Who it's for

  • Trajectory engineers designing transfers and insertions.
  • Mission analysts building Δv budgets for new missions.
  • Flight dynamics engineers planning manoeuvres in operations.
  • Propulsion systems engineers sizing propellant for transfers.
  • Trajectory optimisation researchers.
  • Manoeuvre operations engineers at satellite operators.
  • Engineering or science graduates looking to enter the space industry.
Standards & tools

What you'll work with

  • ECSS-E-ST-10-09C (reference coordinate system)
  • CCSDS 502.0-B (Orbit Data Messages) (standard formats for orbit data exchange)
  • ECSS-E-ST-60-30C (satellite attitude and orbit control system requirements)
  • ECSS-E-ST-35C (space propulsion general requirements)
  • ISO 24113 (space debris mitigation requirements)
  • ECSS-E-ST-10C (system engineering general requirements)
  • GMAT
  • pykep
  • Orekit
  • MATLAB
  • CasADi
Syllabus

6 modules

  1. 1.1The impulsive manoeuvre assumption
  2. 1.2The Tsiolkovsky equation
  3. 1.3Tangential and radial velocity changes
  4. 1.4Plane change manoeuvres
  5. 1.5Combined manoeuvres
  6. 1.6Gravity and finite-thrust losses
  7. 1.7Mission Δv budget
  8. 1.8Efficiency of manoeuvres at periapsis
  9. 1.9Manoeuvre execution errors
  10. 1.10Workshop: Δv calculation for an orbit insertion
  1. 2.1Hohmann transfer
  2. 2.2Bi-elliptic transfer
  3. 2.3Hohmann versus bi-elliptic comparison
  4. 2.4Transfers between elliptical orbits
  5. 2.5Phasing and orbital rendezvous
  6. 2.6Transfer time
  7. 2.7GTO to GEO transfer
  8. 2.8Semi-major axis and eccentricity adjustment
  9. 2.9Three-impulse transfers
  10. 2.10Practical: Hohmann transfer in GMAT
  1. 3.1Formulation of Lambert's problem
  2. 3.2Izzo and Battin algorithms
  3. 3.3Porkchop plots
  4. 3.4Interplanetary transfers
  5. 3.5Sphere of influence and patched conics
  6. 3.6Gravity assists
  7. 3.7Characteristic energy C3
  8. 3.8Launch windows
  9. 3.9Free-return trajectories
  10. 3.10Lab: Earth-Mars porkchop plot
  1. 4.1Gauss's variational equations
  2. 4.2Continuous-thrust spirals
  3. 4.3Edelbaum approximation
  4. 4.4Q-law guidance laws
  5. 4.5Time and mass optimisation
  6. 4.6Electric orbit raising
  7. 4.7Combining high and low thrust
  8. 4.8Effect of eclipses on the transfer
  9. 4.9Thrust direction optimisation
  10. 4.10Case study: orbit-raising spiral to GEO with Edelbaum
  1. 5.1Optimal control and Pontryagin's principle
  2. 5.2Direct and collocation methods
  3. 5.3Single and multiple shooting
  4. 5.4Nonlinear programming
  5. 5.5Operational constraints
  6. 5.6Sensitivity to execution errors
  7. 5.7Trajectory correction
  8. 5.8Optimisation tools
  9. 5.9Visibility and operations constraints
  10. 5.10Case study: optimisation of a constrained transfer
  1. 6.1Definition of initial and final orbits
  2. 6.2Analysis of impulsive alternatives
  3. 6.3Low-thrust study
  4. 6.4Trajectory optimisation
  5. 6.5Δv and propellant budget
  6. 6.6Execution error analysis
  7. 6.7Manoeuvre plan
  8. 6.8Comparison of solutions
  9. 6.9Report and presentation
  10. 6.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

100% online training on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within each intake, so the programme is compatible with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is GMAT, pykep, Orekit, MATLAB and CasADi, in free, academic or evaluation versions. Testing is studied through real procedures: a Hohmann transfer from LEO to GEO, a porkchop plot for an interplanetary mission, and optimisation of a low-thrust spiral. Assessment is continuous by module, plus the final project.

Standards covered: ECSS-E-ST-10-09C, CCSDS 502.0-B (Orbit Data Messages), ECSS-E-ST-60-30C, ECSS-E-ST-35C, ISO 24113, ECSS-E-ST-10C.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of ECSS-E-ST-10-09C, CCSDS 502.0-B (Orbit Data Messages) and ECSS-E-ST-60-30C applied to real cases, not as a theoretical annex.
Industry software:GMAT, pykep, Orekit, MATLAB and CasADi, in free, academic or evaluation versions.
Final project:a manoeuvre plan for a real mission, from impulsive and low-thrust alternatives to trajectory optimisation, Δv and propellant budget and execution error analysis, reviewed by your tutor.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Orbit insertion Δv
Calculate the Δv for an orbit insertion manoeuvre.
Hohmann transfer
Model a Hohmann transfer from LEO to GEO in GMAT.
Porkchop plot
Build an Earth-Mars porkchop plot by solving Lambert's problem.
Low-thrust spiral
Optimise a low-thrust orbit-raising spiral to GEO.
Final project
Prepare a manoeuvre plan for a real mission, reviewed by your tutor.
Career opportunities

Where this takes you

Trajectory engineerMission analystFlight dynamics engineerPropulsion systems engineerTrajectory optimisation researcherManoeuvre operations engineer
Admissions & scholarships

Requirements

  • No prior qualification is required.
  • Internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 300 hours over 3 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with GMAT, pykep, Orekit, MATLAB and CasADi, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute certificate, awarded on passing the continuous assessment and the final project. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed are recognised in a higher programme in the same area (postgraduate diploma or master's). Ask about the recognition policy when you enrol.

No prior qualification is required; you need a computer able to run the programme software and English sufficient to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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