Copyright © Philip M. Parker, INSEAD. Terms of Use.
| Domain | Definition |
Aerospace | A method of ignition of a liquid-propellant rocket engine in which a liquid which is hypergolic with either the fuel or the oxidizer is injected into the combustion chamber to initiate combustion.Aniline is used as an auxiliary fluid with nitric acid and some organic fuels to initiate combustion. (references) |
Source: compiled by the editor from various references; see credits. | |
Hexadecimal (or equivalents, 770AD-1900s) (references)41 55 58 49 4C 49 41 52 59 46 4C 55 49 44 49 47 4E 49 54 49 4F 4E |
| Leonardo da Vinci (1452-1519; backwards) (references)
|
Binary Code (1918-1938, probably earlier) (references)01000001 01010101 01011000 01001001 01001100 01001001 01000001 01010010 01011001 00100000 01000110 01001100 01010101 01001001 01000100 00100000 01001001 01000111 01001110 01001001 01010100 01001001 01001111 01001110 |
HTML Code (1990) (references)A U X I L I A R Y   F L U I D   I G N I T I O N |
ISO 10646 (1991-1993) (references)0041 0055 0058 0049 004C 0049 0041 0052 0059 0046 004C 0055 0049 0044 0049 0047 004E 0049 0054 0049 004F 004E |
Encryption (beginner's substitution cypher): (references)3555584346433552592404655433824341484354434948 |
| 1. Orthography 2. Bibliography |
Copyright © Philip M. Parker, INSEAD. Terms of Use.
