Special modeling techniques were developed to simulate an accurate mathematical model of the transporter/canister/payload system during ground transport of the Inertial Upper Stage/Tracking and Data Relay Satellite (IUS/TDRS) payload. The three finite element models - the transporter, the canister, and the IUS/TDRS payload - were merged into one model and used along with the NASTRAN normal mode analysis. Deficiencies were found in the NASTRAN program that make a total analysis using modal transient response impractical. It was also discovered that inaccuracies may exist for NASTRAN rigid body modes on large models when Given's method for eigenvalue extraction is employed. The deficiencies as well as recommendations for improving the NASTRAN...
The natural frequencies and mode shapes of a 1/15 scale space shuttle dynamics model are analyticall...
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
The measurements taken during the Ares I-X test flight provided a unique opportunity to assess the a...
The space shuttle configuration has more complex structural dynamic characteristics than previous la...
A significant part of the flight readiness verification process involves transient analysis of the c...
A 1/8-scale structural dynamics model of the space shuttle orbiter was analyzed using the NASA Struc...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
Data measurement and interpretation techniques were defined for application to the first few space s...
Previously developed dynamic models for the calculation of lift-off dynamic response of the space sh...
Described here is a method for determining the transient response of, and the resultant loads in, a ...
Matrix form of equations of motion used in iterative processes for determining normal modes and freq...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
Present analytical techniques by which design loads are predicted are very costly and time consuming...
The Tethered Satellite System Mission was analyzed to determine its impacts on the Mission Control C...
In March 2006, the Tracking and Data Relay Satellite (TDRS)-3 experienced an unexpected thrusting ev...
The natural frequencies and mode shapes of a 1/15 scale space shuttle dynamics model are analyticall...
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
The measurements taken during the Ares I-X test flight provided a unique opportunity to assess the a...
The space shuttle configuration has more complex structural dynamic characteristics than previous la...
A significant part of the flight readiness verification process involves transient analysis of the c...
A 1/8-scale structural dynamics model of the space shuttle orbiter was analyzed using the NASA Struc...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
Data measurement and interpretation techniques were defined for application to the first few space s...
Previously developed dynamic models for the calculation of lift-off dynamic response of the space sh...
Described here is a method for determining the transient response of, and the resultant loads in, a ...
Matrix form of equations of motion used in iterative processes for determining normal modes and freq...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
Present analytical techniques by which design loads are predicted are very costly and time consuming...
The Tethered Satellite System Mission was analyzed to determine its impacts on the Mission Control C...
In March 2006, the Tracking and Data Relay Satellite (TDRS)-3 experienced an unexpected thrusting ev...
The natural frequencies and mode shapes of a 1/15 scale space shuttle dynamics model are analyticall...
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
The measurements taken during the Ares I-X test flight provided a unique opportunity to assess the a...