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MIL-HDBK-340A VOL II
TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES VOL II: APPLICATIONS GUIDELINES
Year: 1999
Abstract: This Volume II of the handbook provides additional information pertaining to the test requirements of the handbook, "test requirements for launch, upper stage and space vehicles".
This Vol II of the Handbook was written to provide explanations and guidance to the users of VOL I of the Handbook. The information presented herein is intended to aid in the formulation and review of detailed test requirements for launch, upper stage and space vehicles including the tailoring of VOL I of the Handbook requirements for specific program specifications or contracts.
The organization of this handbook differs from that in VOL I of the Handbook where test requirements for specific levels of hardware assembly are individually discussed for each test category such as acoustics, vibration, thermal vacuum and thermal cycling. The organization of Vol II is structured to allow for a discussion of each test category covering the same type of test at all levels of hardware assembly. For example, the discussion of thermal vacuum testing contains an integrated discussion of thermal vacuum testing and the considerations when these tests are performed at the unit, subsystem and system levels of assembly. The same is true for all other test disciplines addressed in VOL I of the Handbook such as vibration, acoustics, shock, static loads, EMC, pressure, and acceleration.
The documents below are not necessarily all of the referenced herein, but are the ones that are needed in order to fully understand the information provided by this handbook.
The following standards and specifications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solictation. When this handbook is used by acquisition, the application issue of the DoDISS must be cited in the soliciation.
(Unless otherwise indicated, copies of federal and military specifications, standards and handbooks are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)
1. Space and Missile System Center, Los Angeles Air Force Base, El Segundo, CA, "Critical Process Assessment Tool (CPAT), Test and Evaulation, August 1998.
2. Laube, R.B., "Methods To Assess The Success Of Test Programs" The Aerospace Corporation, Proceedings of the 7th Aerospace Testing Seminar - Institute of Environmental Sciences, October 1982.
3. Hamberg, O.; Brackin, C.A.; Tosney, W.F., "Satellite Environmental Testing Cost Benefits" The Aerospace Corporation, Proceedings of the 12th Aerospace Testing Seminar - Institute of Environmental Sciences, March 1990.
4. Hamberg, O.; Tosney, W.F.; Brackin, C.A., "The Effectiveness and Cost Benefits of Satellite Environmental Acceptance Tests" The Aerospace Corporation, Proceedings of the International Symposium on Environmental Testing for Space Programmes ESTEC, Noordwjik, The Netherlands, June 1990.
5. Moening, C.J.; Rubin, S., "An Overview of DoD Test Requirements For Launch and Space Systems" The Aerospace Corporation, Proceedings of the NATO Advisory Group for Aerospace Research and Development (AGARD) Flight Vehicle Integration Panel Symposium, Cannes, France October 1994.
6. Himelblau, H., Piersol, A.G., Grundvig, M.R., Wise, J.H., "Handbook of Dynamic Data Acquisition and Analysis," Institute of Environmental Sciences, IES-RP-DTE012.1, 1994.
7. Gilmore, D.G. (Editor) "Satellite Thermal Control Handbook," The Aerospace Corporation, 1994.
8. Craig, R.R., Bampton, M.C.C., "Coupling of Substructures for Dynamic Analyses," AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1313-1319.
9. Hurty, W.C., "Dynamic Analysis of Structural Systems Using Component Modes," AIAA Journal, Vol. 3, No. 4, April 1965, pp. 1152-1154..
10. Benfield, W.A., Hruda, R.F., "Vibration analysis of Structure by Component Mode Substitution," AIAA Journal, Vol. 9, No. 7, July 1971, pp. 1255-1261.
11. Guyan, R.J., "Reduction of Stiffness and Mass Matrices," AIAA Journal, Vol. 3, No. 2, February 1965
12. Kientzy, D. And Richardson M., "Using Finite Element Data to Set Up Modal Tests", Sound and Vibration, June 1989, pp 16-23.
In the event of a conflict between the text of this document and the references sited herein, the text of this document takes precedence. Nothing in this document, however, supercedes applicable laws and regulations unless a specific exemption has been obtained.
This Vol II of the Handbook was written to provide explanations and guidance to the users of VOL I of the Handbook. The information presented herein is intended to aid in the formulation and review of detailed test requirements for launch, upper stage and space vehicles including the tailoring of VOL I of the Handbook requirements for specific program specifications or contracts.
The organization of this handbook differs from that in VOL I of the Handbook where test requirements for specific levels of hardware assembly are individually discussed for each test category such as acoustics, vibration, thermal vacuum and thermal cycling. The organization of Vol II is structured to allow for a discussion of each test category covering the same type of test at all levels of hardware assembly. For example, the discussion of thermal vacuum testing contains an integrated discussion of thermal vacuum testing and the considerations when these tests are performed at the unit, subsystem and system levels of assembly. The same is true for all other test disciplines addressed in VOL I of the Handbook such as vibration, acoustics, shock, static loads, EMC, pressure, and acceleration.
The documents below are not necessarily all of the referenced herein, but are the ones that are needed in order to fully understand the information provided by this handbook.
The following standards and specifications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solictation. When this handbook is used by acquisition, the application issue of the DoDISS must be cited in the soliciation.
Military Standards MIL-STD-810 Environmental Test Methods and Engineering Guidelines MIL-STD-1522 (USAF) Standard General Requirements for Safe Design and Operation of Pressurized Missile and Space Systems MIL-STD-1540D Product Verification Requirements for Launch, Upper Stage and Space Vehicles Handbooks MIL-HDBK-340A Vol I Test Requirements for Launch, Upper Stage, and Space Vehicles: Baselines MIL-HDBK-343 Design, Construction, and Testing Requirements for One-of-a-Kind Space Equipment MIL-HDBK-83575 General Handbook for Space Vehicle Wiring Harness Design and Testing MIL-HDBK-83578 Criteria for Explosives Systems and Devices Used on Space Vehicles
(Unless otherwise indicated, copies of federal and military specifications, standards and handbooks are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)
1. Space and Missile System Center, Los Angeles Air Force Base, El Segundo, CA, "Critical Process Assessment Tool (CPAT), Test and Evaulation, August 1998.
2. Laube, R.B., "Methods To Assess The Success Of Test Programs" The Aerospace Corporation, Proceedings of the 7th Aerospace Testing Seminar - Institute of Environmental Sciences, October 1982.
3. Hamberg, O.; Brackin, C.A.; Tosney, W.F., "Satellite Environmental Testing Cost Benefits" The Aerospace Corporation, Proceedings of the 12th Aerospace Testing Seminar - Institute of Environmental Sciences, March 1990.
4. Hamberg, O.; Tosney, W.F.; Brackin, C.A., "The Effectiveness and Cost Benefits of Satellite Environmental Acceptance Tests" The Aerospace Corporation, Proceedings of the International Symposium on Environmental Testing for Space Programmes ESTEC, Noordwjik, The Netherlands, June 1990.
5. Moening, C.J.; Rubin, S., "An Overview of DoD Test Requirements For Launch and Space Systems" The Aerospace Corporation, Proceedings of the NATO Advisory Group for Aerospace Research and Development (AGARD) Flight Vehicle Integration Panel Symposium, Cannes, France October 1994.
6. Himelblau, H., Piersol, A.G., Grundvig, M.R., Wise, J.H., "Handbook of Dynamic Data Acquisition and Analysis," Institute of Environmental Sciences, IES-RP-DTE012.1, 1994.
7. Gilmore, D.G. (Editor) "Satellite Thermal Control Handbook," The Aerospace Corporation, 1994.
8. Craig, R.R., Bampton, M.C.C., "Coupling of Substructures for Dynamic Analyses," AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1313-1319.
9. Hurty, W.C., "Dynamic Analysis of Structural Systems Using Component Modes," AIAA Journal, Vol. 3, No. 4, April 1965, pp. 1152-1154..
10. Benfield, W.A., Hruda, R.F., "Vibration analysis of Structure by Component Mode Substitution," AIAA Journal, Vol. 9, No. 7, July 1971, pp. 1255-1261.
11. Guyan, R.J., "Reduction of Stiffness and Mass Matrices," AIAA Journal, Vol. 3, No. 2, February 1965
12. Kientzy, D. And Richardson M., "Using Finite Element Data to Set Up Modal Tests", Sound and Vibration, June 1989, pp 16-23.
In the event of a conflict between the text of this document and the references sited herein, the text of this document takes precedence. Nothing in this document, however, supercedes applicable laws and regulations unless a specific exemption has been obtained.
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MIL-HDBK-340A VOL II
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| contributor author | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) | |
| date accessioned | 2017-09-04T17:49:27Z | |
| date available | 2017-09-04T17:49:27Z | |
| date copyright | 04/01/1999 | |
| date issued | 1999 | |
| identifier other | EUBOIAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/172714 | |
| description abstract | This Volume II of the handbook provides additional information pertaining to the test requirements of the handbook, "test requirements for launch, upper stage and space vehicles". This Vol II of the Handbook was written to provide explanations and guidance to the users of VOL I of the Handbook. The information presented herein is intended to aid in the formulation and review of detailed test requirements for launch, upper stage and space vehicles including the tailoring of VOL I of the Handbook requirements for specific program specifications or contracts. The organization of this handbook differs from that in VOL I of the Handbook where test requirements for specific levels of hardware assembly are individually discussed for each test category such as acoustics, vibration, thermal vacuum and thermal cycling. The organization of Vol II is structured to allow for a discussion of each test category covering the same type of test at all levels of hardware assembly. For example, the discussion of thermal vacuum testing contains an integrated discussion of thermal vacuum testing and the considerations when these tests are performed at the unit, subsystem and system levels of assembly. The same is true for all other test disciplines addressed in VOL I of the Handbook such as vibration, acoustics, shock, static loads, EMC, pressure, and acceleration. The documents below are not necessarily all of the referenced herein, but are the ones that are needed in order to fully understand the information provided by this handbook. The following standards and specifications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solictation. When this handbook is used by acquisition, the application issue of the DoDISS must be cited in the soliciation. Military Standards MIL-STD-810 Environmental Test Methods and Engineering Guidelines MIL-STD-1522 (USAF) Standard General Requirements for Safe Design and Operation of Pressurized Missile and Space Systems MIL-STD-1540D Product Verification Requirements for Launch, Upper Stage and Space Vehicles Handbooks MIL-HDBK-340A Vol I Test Requirements for Launch, Upper Stage, and Space Vehicles: Baselines MIL-HDBK-343 Design, Construction, and Testing Requirements for One-of-a-Kind Space Equipment MIL-HDBK-83575 General Handbook for Space Vehicle Wiring Harness Design and Testing MIL-HDBK-83578 Criteria for Explosives Systems and Devices Used on Space Vehicles (Unless otherwise indicated, copies of federal and military specifications, standards and handbooks are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 1. Space and Missile System Center, Los Angeles Air Force Base, El Segundo, CA, "Critical Process Assessment Tool (CPAT), Test and Evaulation, August 1998. 2. Laube, R.B., "Methods To Assess The Success Of Test Programs" The Aerospace Corporation, Proceedings of the 7th Aerospace Testing Seminar - Institute of Environmental Sciences, October 1982. 3. Hamberg, O.; Brackin, C.A.; Tosney, W.F., "Satellite Environmental Testing Cost Benefits" The Aerospace Corporation, Proceedings of the 12th Aerospace Testing Seminar - Institute of Environmental Sciences, March 1990. 4. Hamberg, O.; Tosney, W.F.; Brackin, C.A., "The Effectiveness and Cost Benefits of Satellite Environmental Acceptance Tests" The Aerospace Corporation, Proceedings of the International Symposium on Environmental Testing for Space Programmes ESTEC, Noordwjik, The Netherlands, June 1990. 5. Moening, C.J.; Rubin, S., "An Overview of DoD Test Requirements For Launch and Space Systems" The Aerospace Corporation, Proceedings of the NATO Advisory Group for Aerospace Research and Development (AGARD) Flight Vehicle Integration Panel Symposium, Cannes, France October 1994. 6. Himelblau, H., Piersol, A.G., Grundvig, M.R., Wise, J.H., "Handbook of Dynamic Data Acquisition and Analysis," Institute of Environmental Sciences, IES-RP-DTE012.1, 1994. 7. Gilmore, D.G. (Editor) "Satellite Thermal Control Handbook," The Aerospace Corporation, 1994. 8. Craig, R.R., Bampton, M.C.C., "Coupling of Substructures for Dynamic Analyses," AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1313-1319. 9. Hurty, W.C., "Dynamic Analysis of Structural Systems Using Component Modes," AIAA Journal, Vol. 3, No. 4, April 1965, pp. 1152-1154.. 10. Benfield, W.A., Hruda, R.F., "Vibration analysis of Structure by Component Mode Substitution," AIAA Journal, Vol. 9, No. 7, July 1971, pp. 1255-1261. 11. Guyan, R.J., "Reduction of Stiffness and Mass Matrices," AIAA Journal, Vol. 3, No. 2, February 1965 12. Kientzy, D. And Richardson M., "Using Finite Element Data to Set Up Modal Tests", Sound and Vibration, June 1989, pp 16-23. In the event of a conflict between the text of this document and the references sited herein, the text of this document takes precedence. Nothing in this document, however, supercedes applicable laws and regulations unless a specific exemption has been obtained. | |
| language | English | |
| title | MIL-HDBK-340A VOL II | num |
| title | TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES VOL II: APPLICATIONS GUIDELINES | en |
| type | standard | |
| page | 121 | |
| status | Active | |
| tree | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;1999 | |
| contenttype | fulltext |