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Automotive
Aviation
Railroad
Shipbuilding
Defense
Services
Overview of services
Lightweight construction consulting
Calculation
Construction
Technical weight management
Cost analysis and optimization
Technology consulting
Software
Knowledge
Academy
Lightweight construction glossary
Innovations
Bionic vault structuring
Modular starter battery (LBSB)
Ebase - Sliding bay frame system
Lightweight heat exchanger (LHE)
Lightweight equipment container system (LGS)
About us
Contact us
Industry Sectors
Automotive
Aviation
Railroad
Shipbuilding
Defense
Services
Overview of services
Lightweight construction consulting
Calculation
Construction
Technical weight management
Cost analysis and optimization
Technology consulting
Software
Knowledge
Academy
Lightweight construction glossary
Innovations
Bionic vault structuring
Modular starter battery (LBSB)
Ebase - Sliding bay frame system
Lightweight heat exchanger (LHE)
Lightweight equipment container system (LGS)
About us
Contact us
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Lightweight construction glossary
Axle load
Axle load distribution (rail vehicle)
Changes outside the scope of application
Design load case
Pending change to the mass properties
Ballast
Base weight
Stress and resilience
Loading model
Reporting on mass properties
Proof of operational stability
Operating empty weight
Operating mass with normal payload (MNO)
Operating mass in operational condition (MVO)
Bottom-Up & Top-Down
Opportunities for weight reduction
COG Envelope
COG range (Center of Gravity Range) of an aircraft
Curb weight (DIN empty weight)
The maximum take-off weight
The maximum empty tank weight
Database for mass properties
The mean aerodynamic wing depth (MAC)
Dynamic strength
Properties of the calculated mass
Properties of the estimated mass
Properties of the critical mass
Permitted mass increase
Test axle load
Vehicle weight
Spring force/ spring load
Flight range limit
Total weight
Weight and center of gravity control
Weight breakup
Weight control
Weight management
Weight distribution
Base mass
Empty manufacturer weight
Maximum load
Changes within the scope of application
Inert mass
Landing weight
Load distribution
Empty weight
Empty mass
Mass properties
Mass control
Mass limitation
Mass management/engineering
Center of mass
Mass reserve
Center of mass
Mass margin
Mass status report
Mass distribution (general)
Mass distribution (airplane)
Maximum landing weight
Maximum weight
Multi-body simulation
Possible change
Verification program
Payload for spacecraft
Payload aircraft
Payload range
Forecast weight
Forecasted mass
Predicted payload capacity
Wheel load
Ramp weight
Space system
Spacecraft
Mathematical proof of strength
Maturity levels of masses
Residual fuel
Risks and opportunities
Risk and potential management
Satellite
Focus
Center of gravity of an aircraft
Shift in center of gravity (aerospace)
Static strength
Controlling the mass properties of aircraft and spacecraft
Symmetry of the load distribution
Actual mass properties
Tolerances
Carrier rocket
Moment of inertia
Dry matter
Overruns
Uncertainty
VDV guidelines
Vector of the target state
Use of trim weights
Predicted mass
Zero Fuel Weight
Target weight
Target mass
Payload
Permissible axle load
Permissible mass/ NTEW
Permissible total weight
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