Copyright © Philip M. Parker, INSEAD. Terms of Use.

| Domain | Definition |
Aerospace | (Symbol c*) Of a rocket engine, a descriptive parameter, c* = Ve/CFwhere Ve is effective exhaust velocity and CF is thrust coefficient. Also called characteristic velocity. (references) |
Source: compiled by the editor from various references; see credits. | |
Crosswords: CHARACTERISTIC EXHAUST VELOCITY |
| Specialty definitions using "CHARACTERISTIC EXHAUST VELOCITY": characteristic velocity. (references) |
Hexadecimal (or equivalents, 770AD-1900s) (references)43 48 41 52 41 43 54 45 52 49 53 54 49 43      45 58 48 41 55 53 54      56 45 4C 4F 43 49 54 59 |
| Leonardo da Vinci (1452-1519; backwards) (references)
|
Binary Code (1918-1938, probably earlier) (references)01000011 01001000 01000001 01010010 01000001 01000011 01010100 01000101 01010010 01001001 01010011 01010100 01001001 01000011 00100000 01000101 01011000 01001000 01000001 01010101 01010011 01010100 00100000 01010110 01000101 01001100 01001111 01000011 01001001 01010100 01011001 |
HTML Code (1990) (references)C H A R A C T E R I S T I C   E X H A U S T   V E L O C I T Y |
ISO 10646 (1991-1993) (references)0043 0048 0041 0052 0041 0043 0054 0045 0052 0049 0053 0054 0049 0043      0045 0058 0048 0041 0055 0053 0054      0056 0045 004C 004F 0043 0049 0054 0059 |
Encryption (beginner's substitution cypher): (references)374235523537543952435354433723958423555535425639464937435459 |
| 1. Crosswords 2. Orthography 3. Bibliography |
Copyright © Philip M. Parker, INSEAD. Terms of Use.