Add to ORKGWater impact drop tests were performed on the space shuttle solid rocket boosters (SRB). Peak water impact pressures and pressure/time traces were measured for various impact velocities using a two-dimensional, full-scale SRB aft skirt internal ring model. Passive burst disc-type pressure transducers were calibrated for use on flight SRB's. The effects on impact pressure of small ring configuration changes and application of thermal protection system cork layers were found to be negligible
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
A post flight assessment of the Space Shuttle's Solid Rocket Boosters was conducted at the John F. K...
The HD 220 program was created as part of the space shuttle solid rocket booster recovery system def...
The results of water impact loads tests using aft skirt end ring, and mid ring segments of the Space...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
The methodology used to predict full scale space shuttle solid rocket booster (SRB) water impact loa...
A technique is developed to optimize the shuttle solid rocket booster (SRB) design for water impact ...
In support of preflight design loads definition, preliminary water impact scale model are being cond...
This user's manual describes the FORTRAN IV computer program developed to compute the total vertical...
Water impact tests using a 12.5 inch diameter model representing a 8.56 percent scale of the Space S...
The results of the attrition/cost studies which formulated the data base for the recommendation to r...
Tests were conducted to determine how thermal conditions affect space shuttle solid rocket booster (...
Data acquired from tests conducted to determine how thermal conditions affect SRB (Space Shuttle Sol...
Data acquired from the initial series of tests conducted to determine how thermal conditions affect ...
The performance requirements, preliminary designs, and development program plans for an airborne rec...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
A post flight assessment of the Space Shuttle's Solid Rocket Boosters was conducted at the John F. K...
The HD 220 program was created as part of the space shuttle solid rocket booster recovery system def...
The results of water impact loads tests using aft skirt end ring, and mid ring segments of the Space...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
The methodology used to predict full scale space shuttle solid rocket booster (SRB) water impact loa...
A technique is developed to optimize the shuttle solid rocket booster (SRB) design for water impact ...
In support of preflight design loads definition, preliminary water impact scale model are being cond...
This user's manual describes the FORTRAN IV computer program developed to compute the total vertical...
Water impact tests using a 12.5 inch diameter model representing a 8.56 percent scale of the Space S...
The results of the attrition/cost studies which formulated the data base for the recommendation to r...
Tests were conducted to determine how thermal conditions affect space shuttle solid rocket booster (...
Data acquired from tests conducted to determine how thermal conditions affect SRB (Space Shuttle Sol...
Data acquired from the initial series of tests conducted to determine how thermal conditions affect ...
The performance requirements, preliminary designs, and development program plans for an airborne rec...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
A post flight assessment of the Space Shuttle's Solid Rocket Boosters was conducted at the John F. K...
The HD 220 program was created as part of the space shuttle solid rocket booster recovery system def...