Paper information

Paper code

IAC-24,C4,IPB,17,x84963

Room

IP Area (Hall B)

Title

Preliminary design of a throttleable hybrid rocket engine using the A-SOFT principle

abstract

View PDF

Session

IPB. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-24

Type of presentation

interactive

Main author

Mr. Joël Martin, Deutsch Luft und Raumfahrt Zentrum (DLR), Germany