SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III. BOEING MODEL 2707. ENVIRONMENTAL CONTROL SUBSYSTEM SPECIFICATION,
Abstract
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the environmental control subsystem (ECS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described. The ECS consists of air source equipment, air-conditioning equipment, cabin temperature and cabin pressure control equipment, and the air distribution system. The ECS shall provide a comfortable and safe environment for the crew and passengers and shall provide the required cooling for the airplane equipment and cargo areas.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 31, 1966
- Accession Number
- AD0827605
Entities
People
- V. D. Warmbo
Organizations
- Boeing