Tomeki

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

By Mary F. Wadel

0 (0 Ratings)
0 Want to read0 Currently reading0 Have read

Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

-

1-1 of 1 Editions

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

View Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

Language: eng

Published In: 1996

Publisher: National Aeronautics and Space Administration, National Technical Information Service, distributor