Copyright © Philip M. Parker, INSEAD. Terms of Use.
| Domain | Definition |
Aerospace | The reciprocal of the specific impulse, i.e., the required propellant flow to produce one pound of thrust in an equivalent rocket. (references) |
Source: compiled by the editor from various references; see credits. | |
Hexadecimal (or equivalents, 770AD-1900s) (references)53 50 45 43 49 46 49 43 50 52 4F 50 45 4C 4C 41 4E 54 43 4F 4E 53 55 4D 50 54 49 4F 4E |
| Leonardo da Vinci (1452-1519; backwards) (references)
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Binary Code (1918-1938, probably earlier) (references)01010011 01010000 01000101 01000011 01001001 01000110 01001001 01000011 00100000 01010000 01010010 01001111 01010000 01000101 01001100 01001100 01000001 01001110 01010100 00100000 01000011 01001111 01001110 01010011 01010101 01001101 01010000 01010100 01001001 01001111 01001110 |
HTML Code (1990) (references)S P E C I F I C   P R O P E L L A N T   C O N S U M P T I O N |
ISO 10646 (1991-1993) (references)0053 0050 0045 0043 0049 0046 0049 0043 0050 0052 004F 0050 0045 004C 004C 0041 004E 0054 0043 004F 004E 0053 0055 004D 0050 0054 0049 004F 004E |
Encryption (beginner's substitution cypher): (references)535039374340433725052495039464635485423749485355475054434948 |
| 1. Orthography 2. Bibliography |
Copyright © Philip M. Parker, INSEAD. Terms of Use.
