File:Nozzle performance comparison.svg
From KYNNpedia
Size of this PNG preview of this SVG file: 300 × 345 pixels. Other resolutions: 209 × 240 pixels | 417 × 480 pixels | 668 × 768 pixels | 890 × 1,024 pixels | 1,781 × 2,048 pixels.
Original file (SVG file, nominally 300 × 345 pixels, file size: 38 KB)
Summary
| Description |
English: Nozzle performance comparison of Bell and Aerospike Nozzle |
| Date | |
| Source |
D.K. Huzel, D.H. Huang, Design of Liquid Propellant Rocket Engines Second Edition, Washington, DC, 1971. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710019929.pdf |
| Author | D.K. Huzel, D.H. Huang, Vectored by Przemyslaw D. Gacia |
Licensing
|
This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) |  |
 |
Warnings:
|
File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 12:09, 7 July 2017 | | 300 × 345 (38 KB) | wikimediacommons>Przemyslaw D. Gacia | Correction of text presentation. |
File usage
The following page uses this file:
