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Technical Paper

Multi-Layer Framework for Synthesis and Evaluation of Heterogeneous System-of-Systems Composed of Manned and Unmanned Vehicles

2018-10-30
2018-01-1964
The advancement of both sensory and unmanned technology, combined with increased utilization of autonomous platforms in complex teaming scenarios, has created a need for practical design space exploration tools to aid in the synthesis of effective System-of-Systems (SoS). The presented work describes a modular, flexible, and extensible framework, referred to herein as the Technologies and Teaming Evaluation (TATE) framework, for straightforward identification of high-quality SoS, which may include both manned and autonomous elements, through quantitative evaluation of system-level and SoS-level attributes against a set of user-defined reference tasks.
Book

The Standard of Knowledge for the Aviation, Space & Defense Industry Quality Practitioner

2012-01-01
This book provides a detailed description of the process-based body of knowledge (BoK) development methodology, and the expanded Quality BoK for the AS&D industry based on the work processes of the industry. The Standard of Knowledge for the Aviation, Space & Defense Industry Quality Practitioner: The AS&D Quality Body of Knowledge (BoK) Version 1 is based on applied research and peer-review validation of the actual quality-related business processes in the AS&D industry, this BoK provided the basis for ADLI professional certification of quality professionals. Essential to quality professionals, this new publication contains comprehensive business process knowledge, along with illustrations and tables to reinforce subjects.
Technical Paper

A Military Space Plane Candidate

1997-10-01
975630
This paper presents a Military Space Plane design concept. While the current military space plane activity is focused on rocket-powered concepts, the concept presented here is powered by a rocket-based combined cycle engine that uses both rocket and air-breathing engine cycles. The design concept is the reference SSTO design concept used in the NASA HRST ANSER study. The reference concept is a derivative of the NASA air-breathing Access to Space study SSTO design concept. The Access to Space air-breathing vehicle's combined cycle engine was replaced by the Aerojet rocket-based combined cycle engine. The orbital performance capability of the reference design concept is presented for 100 n mi., polar, and 225 n mi., 51 deg. orbits. The sensitivity of GTOW to payload and margin is also presented.
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