The HD 220 program was created as part of the space shuttle solid rocket booster recovery system definition. The model was generated to investigate the damage to SRB components under water impact loads. The random nature of environmental parameters, such as ocean waves and wind conditions, necessitates estimation of the relative frequency of occurrence for these parameters. The nondeterministic nature of component strengths also lends itself to probabilistic simulation. The Monte Carlo technique allows the simultaneous perturbation of multiple independent parameters and provides outputs describing the probability distribution functions of the dependent parameters. This allows the user to determine the required statistics for each output par...
Water impact tests using a 12.5 inch diameter model representing a 8.56 percent scale of the Space S...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...
The results of water impact loads tests using aft skirt end ring, and mid ring segments of the Space...
A technique is developed to optimize the shuttle solid rocket booster (SRB) design for water impact ...
This user's manual describes the FORTRAN IV computer program developed to compute the total vertical...
The methodology used to predict full scale space shuttle solid rocket booster (SRB) water impact loa...
The performance requirements, preliminary designs, and development program plans for an airborne rec...
Ocean surface characteristics at two locations were studied for a space shuttle solid rocket booster...
Water impact drop tests were performed on the space shuttle solid rocket boosters (SRB). Peak water ...
Reusing components from a rocket launch can be cost saving. NASA's space shuttle system has reusable...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
The results of the attrition/cost studies which formulated the data base for the recommendation to r...
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the s...
This users manual for the solid rocket booster performance evaluation model (SRB-II) contains descri...
The state probability technique and the Monte Carlo technique are applied to finding shuttle solid r...
Water impact tests using a 12.5 inch diameter model representing a 8.56 percent scale of the Space S...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...
The results of water impact loads tests using aft skirt end ring, and mid ring segments of the Space...
A technique is developed to optimize the shuttle solid rocket booster (SRB) design for water impact ...
This user's manual describes the FORTRAN IV computer program developed to compute the total vertical...
The methodology used to predict full scale space shuttle solid rocket booster (SRB) water impact loa...
The performance requirements, preliminary designs, and development program plans for an airborne rec...
Ocean surface characteristics at two locations were studied for a space shuttle solid rocket booster...
Water impact drop tests were performed on the space shuttle solid rocket boosters (SRB). Peak water ...
Reusing components from a rocket launch can be cost saving. NASA's space shuttle system has reusable...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
The results of the attrition/cost studies which formulated the data base for the recommendation to r...
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the s...
This users manual for the solid rocket booster performance evaluation model (SRB-II) contains descri...
The state probability technique and the Monte Carlo technique are applied to finding shuttle solid r...
Water impact tests using a 12.5 inch diameter model representing a 8.56 percent scale of the Space S...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...
The results of water impact loads tests using aft skirt end ring, and mid ring segments of the Space...