Add to ORKGThe development of a full scale payload integration method which reduces the cost of a load cycle and is capable of land long very large systems is discussed. The method solves the coupled booster/payload system equations and does not involve additional approximations as compared to the standard transient analysis. The method is cost effective and directly applicable to the shuttle payload design case
The atmospheric ascent flight phase of the mated composite booster and orbiter is discussed. The com...
The vibration, acoustic and low frequency loads data from the first 5 shuttle flights are presented....
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is de...
Present analytical techniques by which design loads are predicted are very costly and time consuming...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
The prediction of flight loads and their potential reduction, using various control system logics fo...
This User Guide with an overview of an integration scheme to determine the response of a launch vehi...
From the beginning of the Shuttle Program to its end, integrated loads and dynamics analyses and tes...
Described here is a method for determining the transient response of, and the resultant loads in, a ...
Loads methods currently being used to design shuttle orbiter payloads are summarized. Methods used f...
A significant part of the flight readiness verification process involves transient analysis of the c...
A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce ...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
Rigid body load relief and modal suppression control systems for space shuttle vehicle
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The atmospheric ascent flight phase of the mated composite booster and orbiter is discussed. The com...
The vibration, acoustic and low frequency loads data from the first 5 shuttle flights are presented....
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is de...
Present analytical techniques by which design loads are predicted are very costly and time consuming...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
The prediction of flight loads and their potential reduction, using various control system logics fo...
This User Guide with an overview of an integration scheme to determine the response of a launch vehi...
From the beginning of the Shuttle Program to its end, integrated loads and dynamics analyses and tes...
Described here is a method for determining the transient response of, and the resultant loads in, a ...
Loads methods currently being used to design shuttle orbiter payloads are summarized. Methods used f...
A significant part of the flight readiness verification process involves transient analysis of the c...
A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce ...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
Rigid body load relief and modal suppression control systems for space shuttle vehicle
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The atmospheric ascent flight phase of the mated composite booster and orbiter is discussed. The com...
The vibration, acoustic and low frequency loads data from the first 5 shuttle flights are presented....
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is de...