SAE AIR 1855A-1995 Actuation System Data Summary for Missiles and Launch Vehicles《导弹和运载车辆的传动系统数据摘要》.pdf

1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDO and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, LVWKHVROHUHVSR

2、QVLELOLWRIWKHXVHU SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 SAE International All rights reserved. No part of this publication may be reproduced,

3、 stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-

4、0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AIR1855A AEROSPACE INFORMATION REPORT AIR1855 REV. A Issued 1985-08 Revised 1995-08 Reaffirmed 2016-09 Superse

5、ding AIR1855 Actuation System Data Summary for Missiles and Launch Vehicles RATIONALE AIR1855A has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE: This SAE Aerospace Information Report (AIR) includes all missile and launch vehicle actuation systems, including electrohydraul

6、ic, electropneumatic, and electromechanical types. The data for many systems are not complete. As more information becomes available, periodic updates will be issued to complete existing data sheets and to add new ones. An index by type of vehicle and by type of actuation system is included. The act

7、ual data sheets in the body of the report are organized in alphabetical order. 1.1 Purpose: A survey of existing designs (past and present) is a valuable aid during the concept formulation stage of a new design. This summary report on missile and launch vehicle actuation systems has been formulated

8、to provide a data base that should be useful in the initial design stages of a new system. 2. REFERENCES: There are no referenced publications specified herein. 3. VEHICLE INDEX: 3.1 Type of Vehicle: SAE INTERNATIONAL AIR1855A Page 2 of 58 3.1.1 Missile: - ACM (Advanced Cruise Missile) - ALCM (Air L

9、aunched Cruise Missile) - AMRAAM (Advanced Medium Range Air-Air Missile) - ASALM (Advanced Strategic Air-Launched Missile) - Condor - Copperhead - Dragon - Falcon (Aim 4D, F and G) - GBU-15 (Guided Bomb Unit) - Harm - Harpoon - Hawk - Hellfire - HOBOS (GBU-8) - Hornet - Maverick - Nike Hercules - Pa

10、triot - Pershing (P-1a) - Phoenix - SIAM - SICBM (Small Intercontinental Ballistic Missile) - Sidewinder - Sparrow - Standard Missile - Stinger Alternate - Talos - Tomahawk (Rocket Motor, Rocket Motor Improved, and Cruise) - TOW (Tube-Launched, Optically Tracked, Wire-Guided) 3.1.2 Booster/Space Veh

11、icle: - Atlas (Booster, Sustainer, Vernier) - Centaur - Delta (1st Stage) - IUS (Inertial Upper Stage) - Titan (1st Stage, 2nd Stage Main and Roll Engines) - Titan IV (SRM Booster) SAE INTERNATIONAL AIR1855A Page 3 of 58 3.1.3 ICBM/ABM: - Minuteman I, II, III (Stages 1, 2, 3) - Peacekeeper (Stages 1

12、 and 3) - Spartan - Sprint (Stages 1 and 2) 3.2 Type of Actuation System: 3.2.1 Hydraulic: - ASALM - Atlas (Booster, Sustainer, Vernier) - Centaur - Delta (1st Stage) - Falcon (Aim 4D, F, and G) - Hawk - Minuteman I, II, III (Stages 1, 2, and 3) - Nike Hercules - Patriot - Peacekeeper (Stages 1 and

13、3) - Pershing (P-1a) - Phoenix - SICBM - Sparrow - Spartan - Sprint (Stages 1 and 2) - Talos - Titan II, III, and IV (1st Stage, 2nd Stage Main and Roll Engines) - Titan IV Solid Rocket Motor Upgrade (SRMU) - Tomahawk (Rocket Motor and Rocket Motor Improved) 3.2.2 Electropneumatic: - Copperhead - Dr

14、agon - GBU-15 - Hellfire - HOBOS (GBU-8) - Hornet - Maverick - SIAM - Sidewinder - Stinger Alternate - TOW SAE INTERNATIONAL AIR1855A Page 4 of 58 3.2.3 Electromechanical: - Advanced Cruise Missile - Air Launched Cruise Missile - AMRAAM (Advanced Development) - ASALM - Condor - Harm - Harpoon/Slam -

15、 IUS - Standard Missile - Titan IV Type I Space Launch Booster - Tomahawk (Cruise) 4. GENERAL NOTES OR DISCLAIMER: In most cases, the data sheets list the original vehicle and actuation system manufacturers. No attempt has been made to keep current all of the listed companies and trace mergers, cons

16、olidations, divestitures, etc. such as the following examples: a. Lockheed Martin is now the vehicle manufacturer for the Atlas and Centaur which prior to the merger was Martin Marietta and previously General Dynamics Convair or GDSS. b. Hughes is the vehicle manufacturer for the Tomahawk previously

17、 done by General Dynamics Convair (McDonnell Douglas is a second source). PREPARED BY THE MISSILE AND SPACE SYSTEMS PANEL OF SAE SUBCOMMITTEE A-6A, FLUID POWER SYSTEMS OF COMMITTEE A-6, AEROSPACE FLUID POWER, ACTUATION & CONTROL TECHNOLOGIES SAE INTERNATIONAL AIR1855A Page 5 of 58 SAE INTERNATIONAL

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