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Load and dynamic assessment of b-52b-008 carrier aircraft for finned configuration 1 space shuttle solid rocket booster decelerator subsystem drop test vehicle. volume 1: summary
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Quade, D. A. |
| Copyright Year | 1978 |
| Description | The B-52B airplane was identified for use in solid rocket booster (RSB) parachute drop flight testing. The purpose of this study was to determine by theoretical analysis methods the compatability and structural capability of B-52B drop test vehicle configuration (with fins) to accomplish the drop test mission. This document consist of four volumes. This volume presents a summary of airplane flutter and load strength evaluation analysis results and a comparative study of the pylon loading resulting from drop test vehicle inertia and aerodynamic considerations. |
| File Size | 1478203 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790001877 |
| Archival Resource Key | ark:/13960/t9b61cm0f |
| Language | English |
| Publisher Date | 1978-06-09 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Test Vehicles Pylon Mounting Drop Tests Parachute Descent Flutter Aerodynamic Characteristics Aircraft Configurations Space Shuttle Boosters Payloads B-52 Aircraft Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
