2000
DOI: 10.2514/2.3534
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Nontangent, Developed Contour Bulkheads for a Single-Stage Launch Vehicle

Abstract: Dry weights for single-stage launch vehicles that incorporate nontangent, developed contour bulkheads are estimated and compared to a baseline vehicle with 1.414 aspect ratio ellipsoidal bulkheads. Weights, volumes, and heights of optimized bulkhead designs are computed using a preliminary design bulkhead analysis code. The dry weights of vehicles that incorporate the optimized bulkheads are predicted using a vehicle weights and sizing code. Two optimization approaches are employed. A structural-level method, … Show more

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Cited by 2 publications
(1 citation statement)
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“…Its high specific strength and stiffness will improve lift efficiency, fuel economy, and performance, and would also increase payload capabilities of air and spacecrafts. This material has also been considered for use in the bulkheads of reusable single-stage-to-orbit launch vehicles [3] and combat ground vehicles [4]. The effects of composition, processing and aging conditions on the microstructure and tensile properties of this material have been extensively studied.…”
Section: Introductionmentioning
confidence: 99%
“…Its high specific strength and stiffness will improve lift efficiency, fuel economy, and performance, and would also increase payload capabilities of air and spacecrafts. This material has also been considered for use in the bulkheads of reusable single-stage-to-orbit launch vehicles [3] and combat ground vehicles [4]. The effects of composition, processing and aging conditions on the microstructure and tensile properties of this material have been extensively studied.…”
Section: Introductionmentioning
confidence: 99%