What is the difference between dry operating mass and dry operating weight in the context of rotorcraft?
What is the formula for converting mass to weight?
What is the difference between dry operating mass and dry operating weight in the context of rotorcraft?
What is the formula for converting mass to weight?
Weight is a force.
Mass is a property of matter. Acceleration makes mass produce a force. Specifically, a mass in the gravitational field of Earth effects a weight force on its support. The relation between both is the gravitational acceleration g, which is standardized to 9.80665 m/s² (approximately 32.174 ft/s²), as in Weight = Mass · g.
The problem occurs due to lazy terminology. In aviation both normally mean the same thing: The reading you would get if you put the empty aircraft onto a large weighing device (scales, or whatever). This is normally given in kilograms (kg) or pounds (lb).
This trouble arises because both of these quantities are actually masses, the weights would be in Newtons (N) or pounds-force (lbf). To transform the mass into a weight you multiply by the local gravity, g, which is usually assumed to be 9.81m/s2.
A similar problem exists when at home: If you weigh yourself on standard bathroom scales you will normally see a value in kilograms (i.e: A mass), but the scales actually measure a force. This means if you use the same scales on another planet you will get a different value in kilograms, which is nonsensical. The same goes for aviation: Weight and mass are being used interchangeably, which is incorrect.
Weight = Mass x Gravity.
In typical aviation terms, in an operational sense, you don't need to worry about mass (unless you're talking about a spacecraft...)