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Quiet STOL research aircraft development program. Teisoon STOL jikkenki kitai kaihatsu sogo hokokusho

Technical Report:

Abstract

The airframe development program of the quiet STOL research aircraft (ASKA) promoted by National Aerospace Laboratory, Japan is reported in detail. ASKA was developed based on a C-1 medium-sized troop and freight transport aircraft for the Air Self-Defence Force, and four turbofan- jet engines were substituted for two previous engines. Its first flight was conducted successfully on Oct. 28, 1985 after 8 year development from 1977 to 1985. The ASKA was developed separately on its airframe, engine and flight, and this report includes every related matter to its airframe. The promotion system, budget and executive system are reported in the second chapter, and the design requirements, safety standard and basic design in the third chapter. Several related tests such as wind tunnel test and flight simulation test are reported in the 4th chapter, and the structure and equipment of ASKA are outlined in the final chapter. The appendix includes the line-up of and discussions in the technical committee, the list of newly developed functional parts, the list of design reports and the list of related tests. 50 refs., 8 figs., 23 tabs.
Authors:
Publication Date:
Jan 01, 1994
Product Type:
Technical Report
Report Number:
NAL-TR-1223
Reference Number:
NEDO-94-930193; EDB-95-022131
Subject:
33 ADVANCED PROPULSION SYSTEMS; AIRCRAFT COMPONENTS; MACHINE PARTS; MECHANICAL STRUCTURES; NOISE POLLUTION ABATEMENT; TURBOFAN ENGINES; DESIGN; SAFETY ENGINEERING; PROGRAM MANAGEMENT; BUDGETS; FLIGHT TESTING; SIMULATION; WIND TUNNELS; ENGINEERING; ENGINES; EQUIPMENT; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY; MANAGEMENT; POLLUTION ABATEMENT; TESTING; TUNNELS; TURBOMACHINERY; UNDERGROUND FACILITIES; 330000* - Advanced Propulsion Systems
OSTI ID:
6678417
Research Organizations:
National Aerospace Lab., Chofu, Tokyo (Japan)
Country of Origin:
Japan
Language:
Japanese
Availability:
Available from National Aerospace Laboratory, 44-1, Shindaiji 7-chome, Chofu, Tokyo, Japan
Submitting Site:
NEDO
Size:
Pages: (135 p)
Announcement Date:

Technical Report:

Citation Formats

Not Available. Quiet STOL research aircraft development program. Teisoon STOL jikkenki kitai kaihatsu sogo hokokusho. Japan: N. p., 1994. Web.
Not Available. Quiet STOL research aircraft development program. Teisoon STOL jikkenki kitai kaihatsu sogo hokokusho. Japan.
Not Available. 1994. "Quiet STOL research aircraft development program. Teisoon STOL jikkenki kitai kaihatsu sogo hokokusho." Japan.
@misc{etde_6678417,
title = {Quiet STOL research aircraft development program. Teisoon STOL jikkenki kitai kaihatsu sogo hokokusho}
author = {Not Available}
abstractNote = {The airframe development program of the quiet STOL research aircraft (ASKA) promoted by National Aerospace Laboratory, Japan is reported in detail. ASKA was developed based on a C-1 medium-sized troop and freight transport aircraft for the Air Self-Defence Force, and four turbofan- jet engines were substituted for two previous engines. Its first flight was conducted successfully on Oct. 28, 1985 after 8 year development from 1977 to 1985. The ASKA was developed separately on its airframe, engine and flight, and this report includes every related matter to its airframe. The promotion system, budget and executive system are reported in the second chapter, and the design requirements, safety standard and basic design in the third chapter. Several related tests such as wind tunnel test and flight simulation test are reported in the 4th chapter, and the structure and equipment of ASKA are outlined in the final chapter. The appendix includes the line-up of and discussions in the technical committee, the list of newly developed functional parts, the list of design reports and the list of related tests. 50 refs., 8 figs., 23 tabs.}
place = {Japan}
year = {1994}
month = {Jan}
}