Master

In Maynard (USA)

£ 5,000 + VAT

Description

  • Type

    Master

  • Location

    Maynard (USA)

  • Start date

    Different dates available

This class focuses on chemical rocket propulsion systems for launch, orbital, and interplanetary flight. It studies the modeling of solid, liquid-bipropellant, and hybrid rocket engines. Thermochemistry, prediction of specific impulse, and nozzle flows including real gas and kinetic effects will also be covered. Other topics to be covered include structural constraints, propellant feed systems, turbopumps, and combustion processes in solid, liquid, and hybrid rockets.

Facilities

Location

Start date

Maynard (USA)
See map
02139

Start date

Different dates availableEnrolment now open

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Subjects

  • Systems

Course programme

This course builds on the rocket propulsion portion of 16.50, and adds depth in the disciplines and trade-offs related to chemical rockets. A companion course, 16.522, covers the area of electric rockets, plus those small chemical rockets used for satellite propulsion.


Lectures: 3 sessions / week, 1 hour / session


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Rocket propulsion

£ 5,000 + VAT