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KARI PROPRIETARY 

 
 

KARI PROPRIETARY 

 

Request For Proposal 

 

 

 

 

Shaker Power 

Amplifier System 

for V964 

 

 

 

August, 2010 

 

Space Environment Test Dept. 

Korea Aerospace Research Institute 

 

45 Eoeun-Dong, Yusong-Gu, Daejon, 305-333, Korea 

Phone : 82-42-860-2562, Fax : 82-42-860-2234 

 


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KARI PROPRIETARY 

 
 

KARI PROPRIETARY 

Request For Proposal 

For 

Shaker Power Amplifier System 

for V964 

 

 

 

 

 

 

 

 

 

August, 2010 

 

Space Environment Test Dept. 

Korea Aerospace Research Institute 

 

45 Eoeun-Dong, Yusong-Gu, Daejon, 305-333, Korea   

Phone : 82-42-860-2562, Fax : 82-42-860-2234 

IMPORTANT 

 

1. This RFP shall be kept in confidentiality and shall neither be copied nor 

distributed to the third parties. 

2. The questions on this RFP can be asked to the Space Test Department 

before submission of the proposal. 

3. This RFP shall be returned to Korea Aerospace Research Institute with 

bidder’s proposal. 

4. This RFP shall be legal bind after the contract is awarded unless the bidder   

explicitly expresses the differences from the RFP in the compliance sheet. 


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Table of Contents 

 

II.

 

OVERVIEW.......................................................................................................................... 1

 

1.

  OVERVIEW OF THE PROJECT ..................................................................................................... 1 

2.

  PROCEDURES OF THE PROJECT ................................................................................................. 2 

3.

  REQUISITES OF PARTICIPANTS .................................................................................................. 3 

4.

  SCOPE OF THE CONTRACT ........................................................................................................ 3 

III.

  TECHNICAL REQUIREMENTS ...................................................................................... 4 

1.

  TOTAL SYSTEM CONFIGURATION ............................................................................................. 4 

2.

  GENERAL REQUIREMENTS ....................................................................................................... 6 

3.

  REQUIREMENTS FOR POWER AMPLIFIER .................................................................................. 8 

4.

  REQUIREMENTS FOR COOLING UNITS/FILED POWER SUPPLY ................................................. 11 

5.

  REMOTE CONTROLLER .......................................................................................................... 13 

6.

  MECHANICAL INTERFACE REQUIREMENTS ............................................................................. 15 

7.

  AUXILIARY REQUIREMENTS ................................................................................................... 16 

VI.

  WARRANTY, MAINTENANCE AND OTHER REQUIREMENTS .............................. 1 

1.

  WARRANTY ............................................................................................................................. 1 

2.

  MAINTENANCE ........................................................................................................................ 1 

3.

  ACCEPTANCE ........................................................................................................................... 4 

VII.

  TERMS AND CONDITIONS .............................................................................................. 1 

VIII.

 

FORMAT OF PROPOSAL .............................................................................................. 1

 

 


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II. 

OVERVIEW 

 

1.  Overview of the project 

 

1.1 

Korea Aerospace Research Institute (hereinafter referred to as “KARI”) is located at 

Daeduk Research Complex, 140 km south of Seoul. 

 

1.2 

KARI has a satellite assembly, integration and test center (hereinafter referred to as 

“AITC”) for joint use by corporations and research institutes for the purpose of the 

effective development of domestic satellites. And basic facilities and equipment for 

satellite assembly and test have been supplied, installed and used. 

 

1.3 

The purpose of this project is to change the power amplifier system, remote control panel, 

relating signal cable lines and cooling unit/Field power supply in the electro-magnetic 

shaker system (LDS, V964) in order to maintain the shaker performance and to reinforce 

the interchange with other existing vibration system(V984 & V994 system).   

 

1.4 

The power amplifier system should be combined with the existing shaker components of 

V964 (e.g. Body of shaker) without modification of existing system. If any modification 

needed, the supplier should supply all of components and additional facility without any 

request of cost. 

 

1.5 

Remote control panel should control the all the shaker components safely and exactly as 

the same function of current system. 

 

1.6 

Power amplifier system should accommodate the existing power modules (LDS power 

amplifier module, Model : LDS DPA-K ). 

 

1.7 

The main undertakings of the project are to perform factory and site acceptance tests, 

install, guarantee quality and training, etc. 

 

1.8 

The supply should submit the business showings of the installing the power amplifier & 

control system for LDS V964.   

 

1.9 

All the descriptions in this RFP are minimum requirements and the supplier can suggest 

the better one to improve the overall performance and cost. But in this case, the proposal 

should clearly indicate the improvements from KARI’s requirements. 


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2.  Procedures of the project   

 

2.1 

The project shall be proceeded with five parts as follows: 

 

1) Organization of power amplifier cabin, remote control panel, cooling unit, field power 

supply 

2) Factory acceptance test & safety plan verification (e.g. General power shut down 

case) with V964 shaker body 

3) Transportation  

4) Installation at KARI 

5) Final acceptance test at KARI according to supplied test procedure & previous test 

results 

 

2.2 

The participants shall submit the detailed work schedule for article 2.1. Specially, the 

work schedule at KARI shall be confirmed by KARI for avoiding overlap with KARI’s 

other test schedules. 

 

2.3 

The format of proposal : 

 

1)  The participants shall submit 6 copies of a detailed proposal to KARI according 

to the format and contents satisfying the requirements stipulated in this RFP. 

2)  The compliance sheet with the requirement of this RFP shall certainly be 

included in the proposal. 

3)  The price of the system shall be broken down. 

4)  The participants shall make out a proposal with their own writing. 

5)  The language shall be English or Korean. 

 

2.4 

The proposal shall be delivered to KARI before the due date for submission. 

 

2.5 

All proposals and documents submitted shall become the property of KARI. 

 

 

 


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3.  Requisites of participants 

 

3.1 

The participants shall supply information about themselves according to the form in Part 

V of this RFP. 

 

3.2 

The participants shall also have experience of installation, operation, arranging, 

integrating and wiring the water-cooling shaker system. 

 

3.3 

The supply should submit the business showings of the installing the power amplifier & 

control system for LDS V964.   

 

 

4.  Scope of the contract 

 

4.1 

The project is on turnkey base and the proposal shall include the following; 

 

1) Engineering work of the equipment 

2) Manufacture, assembly and turnkey delivery of the equipment 

3) Parts and particular instruments necessary to operate the equipment 

4) Installation work and acceptance test at factory & KARI site 

5) Project management, site operation, cooperation with KARI 

6) Basic principle, operation, warranty, maintenance, repair, safety and training for 

the equipment 

7) Relevant books and manuals 

8) Other necessary matters required for acquiring and installing the equipment 

(including checking of AITC building interface and construction) 

9) Changing of signal & power cables from power amp. system to shaker body 

10)  Overall V964 system check for shaker body, cooling units and filed power 

supply 

 

 


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III.  Technical Requirements 

 

 

1.  Total System Configuration 

 

Space environmental test dept. is operating the three shaker systems of 480KN, 280kN, 

80KN. One of these shaker systems, the 80kN shaker system was installed in 1994 and 

now is in the operation. The purpose of project is to change all power amplifier system 

except the shaker body in order to maintain the shaker performance and safety. 

 

Figure 1 Specifications of V964 (80 kN)   

 

The currently installed and operated shaker system is composed of shaker and power 

amplifier system. Power amplifier system is composed of power amplifier, cooling units & 

field power supply, remote controller. 

  Shaker : mechanical system of moving the test objects 

 Power 

Amplifier 

System 

  Power Amplifier :  determination of thrust force in the shaker system, 

modular type system included control cabinet 


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Cooling units and Field power supply : water-cooling units for shaker system 

 Remote 

Controller 

 

Amplifier System

Cooling Unit

Shaker

Remote Control Panel

 

Figure 2 Main components of shaker system   

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


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2. General 

requirements 

 

2.1  The supplied amplifier & cooling units system shall be able to operate in the 

previous shaker configuration (LDS V964).   

 

2.2  The supplier shall have successful experience in installation of water-cooling 

shaker system. 

 

2.3  The supplier shall have successful experience of replacement with power 

amplifier, control system, cooling system and field power supply, which are 

products of participant, for LDS V964 (80KN system). 

 

2.4  The power of the amplifiers will be chosen to enable the maximum thrust to be 

reached in sine mode and random mode 

 

2.5  The supplier should provide the all the accessories, interface components and 

cable lines needed to satisfy the best-performance of LDS V964 shaker system. 

 

2.6  By using the power amplifier module sets supplied by KARI, supplier should 

verify the specification of shaker system (Refer to specification of V964). 

Amplifier system should accommodate some of LDS DPA-K(8KVA module type) 

and operated without any problems. 

 

2.7 

Cable set & data link package should be supplied. 

 

2.8  Remote control panel and related system should be supplied.(Only optical 

connection type is allowed) 

 

2.9 

Interface cable between shaker body & power amplifier module system. 

 

2.10  Supplier should check and solve the noise problem 

 

2.11  Supplier should provide the KARI with the maintenance manual. 

 

2.12  The amplifier system shall act as the system control and monitoring center for 

the vibrators, the vibrator cooling equipment, the field power supply and the 


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external interlocks. All of interlocks should be checked & monitored as same of 

previously system. 

 

2.13  Protection unit accommodate the current shaker errors 

 

2.14  Complete control of existing shaker system from control room using amplifier 

remote control 

 

2.15  Supply the remote control panel system with optical modulate 

 

2.16  A length of cables of 30 m ± 2 m(can be more) will be provided between the 

shaker(s) and the amplifier(s). 

 

2.17  Built-in safety feature shuts down the amplifier in the event that communication 

between the amplifier and Remote Panel is interrupted and general power 

problem. The Emergency Stop switch remains active on both the local and 

remote panels during shaker operation. This Emergency Stop switch is a button 

on the front panel of the RCP9 unit, and a separate hardware unit to be located 

near the PC for the software option.   

 

 

 


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3.  Requirements for Power Amplifier 

 

3.1 

Signal to Noise > 65dB. 

 

3.2 

Supply voltage : three-phased 380 V - 60 Hz (ground). 

 

3.3 

The input voltage for full output power will not exceed 5 V peak. 

 

3.4 

The input impedance should be 10 kΩ nominal. 

 

3.5 

Total harmonic distortion should be less 0.5% at full load with current LDS V964 

system. 

 

3.6 

Input sensitivity should be 1 V rms input for 100V rms output (Compatible with all 

standard controllers). 

 

3.7 

Switching frequency is 150,000 Hz 

 

3.8 

Modulator range is DC to 3,000 HZ 

 

3.9 

Rated output voltage is 100 V rms (Sine option) 

 

3.10  Continuous output current is 80 A rms(sine and random) per 8kVA module 

 

3.11 Transient 

output 

current is 240A for 100ms per 8KVA module 

 

3.12  Full power bandwidth is 20 ~ 3,000Hz 

 

3.13  Shock impulse by switching ON-OFF : 

The maximum allowed peak value of a shock impulse, induced by 

switching ON-OFF the amplifiers shall be less than 0.2g measured at 

the empty shaker armature. 


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Power loss protection : 

 

A protection facility has to be implemented in the amplifier(s) to activate 

immediately a safe shutdown when power fails. 

 

3.14  Maximum D.C. offset voltage : +/- 20 mV DC.   

 

3.15  Electrical safety : 

 

The amplifiers, auxiliary equipment, terminal boxes and cable installation 

shall be compliant with the European safety regulations regarding 
electrical installations “European low voltage directive 73/23/EEC”.
 

Verification of the correct application of the rules shall be part of the 

“works acceptance”, for the manufactured components, and of the “final 
acceptance”, for the electrical installation on site. 

 

3.16  Choice of components with low equivalent series inductance and resistance   

3.17  Optical coupling of logic signals   

3.18  Safety devices and interlocks : 

Any malfunctions of the overall system, which requires a test run abort, shall 

result in a soft shut down of the test run. A soft shut down is a controlled 

decrease of the acceleration down to zero, whereby the accelerations at the 

payload interface do not exceed the specified accelerations. In particular the 

test run abort triggered by mains disturbances or interruption shall be controlled. 

The following internal and external interlocks shall be incorporated in the 

amplifier as a minimum. 

 

 

Internal interlocks on 

 

Supply over-current and excessive ripple 

 

Excessive current in individual power modules 

 

Adjustable limits for output current and voltage 

 

Monitoring of D.C supply output voltages and fuses. 

 

Monitoring of D.C offset of output current 

 

Amplifier excessive air temperature 

 

External interlocks on 

 

Master gain switch position (Amplifier ON only possible when Master 

Gain on zero) 


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Over-travel or over-limit detection   

 

Vibrator armature status 

 

Head Expander status 

 Vibrator 

cooling 

 

External amplifier water cooling (if applicable) 

 

Field power supply 

 Amplifier 

balance 

(amplitude/phase) 

 

Field coil temperature 

 Armature 

temperature 

 

Oil pressure of Head Expander 

 

Vibrator mercury switches 

 

Manual abort (red push button) 

 Auxiliary 

supplies. 

 

3.19  Amplifier Local Control 

The amplifier local control shall comprise the following items : 

 

Indicators for output voltage and current 

 

Illuminated push-buttons for amplifier ON/OFF, auxiliary ON/OFF 

 

Illuminated key switch for local/ remote control 

 

Adjustable trip levels for output over voltage and over current 

 

Re-settable alarms for output over voltage and current, supply over 

current, auxiliary voltages, vibrator over travel, vibrator cooling, field 

power supply, fuses and external trip signal 

 

Amplifier gain control 

 Emergency 

stop 

 

Auxiliary oscillator input if applicable (BNC) 

 

3.20  Amplifier – Vibrator interface 

 

If the present amplifier-vibrator interface is a transformer configuration of 

identical double wound transformers with electrical tap changing on the primary 

windings, the transformers have to be located in one enclosure.   


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4.  Requirements for Cooling units/Filed power supply 

 

4.1  Cooling units and field power supply system accommodate voltage range 380, 

400, 415, 440V 50/60Hz, 480, 500, 520V 60Hz. 

4.2 

Supply input power at full level FPS(field power supply) should less than 70 kW. 

4.3 

Supply input power at economy FPS(field power supply) should less than 40 kW. 

4.4 

FPS full level setting value should be below 

 

 

4.5 

FPS economy level setting value should be below 

 

 

4.6 

Degauss supply value should be below 

 


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5. Remote 

Controller 

 

The existing control-command system has to be modified or replaced. The interfaces with 

the new equipment will be under the contractor’s responsibility. The equipment should be 

installed into the existing 19" cabinets. 

 

5.1  Amplifier remote control 

 

The amplifier remote control shall interface with the KARI - SITC vibration 

control console, composed of LMS equipment. The remote control shall be 

located in the control room on the first floor, and shall have the control and 

monitoring of the vibrator. And the remote control shall therefore be equipped 

per amplifier with the control and monitoring devices as described under 

“Amplifier Local Control” and additionally with: 

 

Phase control equipment 

 

Transformer tap changing device if applicable   

 

Master gain control and input attenuator for low level testing 

 

Control of existing vibrator(s) switch cabinet, if applicable, including shaker 

cooling unit(s) and field power supply(ies). 

 

Additional set of voltage and current measuring converters incl. suitable signal 

conditioning (for additional measurement interface) 

 

External trips equipment. 

 

5.2 

Remote control configuration 

   

The amplifier remote control shall have a control and monitoring module 

subdivided into: 

 

5.3  Gain control unit 

 

The gain control unit shall be able to handle. The customers vibration signal of 

10 volt peak to peak, a frequency range between 5 Hz and 2500 Hz, a signal to 

noise ratio better than 90 dB. The output voltage level and impedance to be 

specified by the supplier. The unit shall therefore be equipped with: 

 An 

insulating 

pre-amplifier. 

 

A low pass filter with a corner frequency of 2500 Hz with a roll-off of 80 

dB/decade. 

 

A front panel mounted selector switch to bypass the filter. 

 


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5.4  Vibrator performance display unit : 

 

The vibrator performance display unit comprising front panel mounted individual 

analogue voltage and current measuring devices (logically grouped per vibrator, 

voltmeter above current meters and adequately labeled or engraved) and 

voltage and current measuring converters to facilitate additional measuring 

outputs. The unit shall be equipped with : 

 

Vibrators voltage indicators with scale 0-100% with respect to the RMS. 

 

Vibrators current indicators with scale 0-100% with respect to the RMS vibrator 

current. 

 

Vibrators voltage converters with single ended buffered output, providing an 

output of 50 mV/Vvibr. 

 

Vibrators current converters with single ended buffered output, provided with the 

following front panel labeled selectable outputs: 66.66 mV/Avibr, 20 mV/Avibr, 

6.66 mV/Avibr and 2 mV/Avibr. 

 

The front panel selector must be lockable. 

 

All converters shall have BNC outputs both on the panel front and rear side. 

 

The shaker body position and shaker moving coil position information have to 

be reported in the control and command system. 

 

 

 

 

 


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6.  Mechanical Interface requirements 

 

6.1  The amplifier system should be installed in the previously installed site of 

amplifier. 

6.2 

The amplifier cabinets shall have free-standing self-supporting frames, which will 

rest on a flat concrete floor. Shims or adjustable feet or rollers shall be 

incorporated if necessary. The bottom part of the amplifier casing should be at 

20 cm from the floor. In case the assembled equipment consists of more than 

one cabinet, the frames shall be aligned and bolted together firmly after 

positioning on site. 

6.3 Enclosures 

  The amplifier cabinets shall have metal enclosures which shall meet the 

protection class IP-44 as described in EN 60529/ IEC529, or better, as 

well as the requirements specified by the “European Electromagnetic 

Immunity Standards” as far as applicable for this purpose. 

  Removable panel sections and doors shall have suitable (lift-out) 

hinges for easy removal.   

  Removable panels and doors shall be positioned in such a way that 

easy access to vital components is guaranteed. 

  Hinges should allow for a door opening of 100

o minimum. 

  All doors in a row should open in the same direction. 

 

6.4 

Panel Internal Wiring and Termination : 

  Equipment internal wiring shall run in metal or plastic cable conduit with 

removable covers. 

  Cables and wires attached to front door mounted equipment or swing-

out racks shall be protected by flexible hoses to prevent damage. 

  Only stranded wire and multi-core cables are allowed. 

  Soldering of stranded wire is not allowed. 

  A wiring identification system shall be provided for all circuit with non-

loosening terminal and wire markers. 

 


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6.5 

External and Interface Cabling : 

  Interface cabling between equipment and external interfaces shall enter 

the enclosures from the bottom for power cables and from the top for 

other cables. 

  Cables should either enter the cabinet through properly sized 

compression type cable glands or clamped to a metal bar for stress 

relief. 

  Cables between interfaces shall run in one length. Joints are not 

permitted. 

  Spare wires of multi-core interface cables shall be put on terminals 

  Cable conductors in excess of 16 mm

2 may directly be connected to the 

components concerned if convenient (e.g.. main switches). 

  Power cables and cables carrying large currents should be kept 

separate from control cables. 

  Power cables and cables carrying dangerous voltage levels shall be 

connected to clearly marked terminals and be separated from other 

terminals by separator plates and labeled covers. 

 

 

6.6 

Noise restriction : 

 

The acoustic noise levels inside the building during amplifier operation shall 

not exceed: 

 

100 dBA in the amplifier room 

 

75 dBA in the control room area on the first floor 

 

90 dBA in the test and hall preparation area. 

 

6.7 Temperature 

 

The maximum temperature of the external surfaces of the amplifiers shall be 

lower than 30 degrees ˚C. 

 

 

7. Auxiliary 

requirements 

 

7.1 

Building accommodation : 

7.2 

The amplifiers shall be installed in the machine room at basement level. 

7.3  The doors on ceiling of basement (2400 x 6000 mm) provide entrance for large 

equipment to this room. 


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7.4 

Two side doors of the machine room are available for equipments entrance, The 

larger one is 2300 x 2300 mm(height x width) and the smaller one is 1500 x 

2000 mm(height x width)   

7.5 

Inside the machine room, the free area for maneuvering the equipment is limited 

by existing equipment, such as vibrator cooling units and field power supplies 

7.6 

The room has no gantry crane or other installed lifting equipment. 

 

 

 

 

 

   

 

 

 


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VI.  Warranty, Maintenance and Other Requirements 

 

 

1. Warranty 

 

 

The system shall be warranted for duration of 2 years from the date of definitive 

acceptance on the site against any operational faults. The date of acceptance is the date 

when the whole system is completely installed and its function is approved perfect in a 

written format by KARI or its representative. 

 

 

The warranty covers the replacement of faulty parts, the labor required for repair, 

traveling cost, and all necessary costs.   

 

 

The contractor or A/S teams in a foreign country shall submit the written plan for repair 

within 3 days while the contractor or A/S teams in Korea shall do it within 2 days after 

the reception of the notification of fault. The contractor or A/S teams in a foreign country 

shall completely finish the repair within 2 weeks after the reception of the notification of 

fault while the contractor or A/S teams in Korea shall do it within 1 week.   

 

 

To meet these requirements, the contractor shall propose a detailed plan for the prompt 

repair in the proposal. The detailed information (location, number of crews, resume, 

phone and FAX numbers, etc.) of the A/S teams (in Korea and foreign countries) shall be 

shown in the proposal and shall be approved by KARI. 

 

 

2. Maintenance 

 

2.1 General 

Rules 

 

All parts requiring reconditioning or maintenance must be easily accessible.  Their 

installation and removal must be easy : i.e. 

  the installation and removal shall be possible with standard tooling or 

provided specific handling tooling, 

  visual checks must not be obstructed (lighting shall be provided if 

required), 

  Removal must be performed in perfect safety (electric shocks, high 

voltage, water pressure, compressed air, etc.) 


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All the parts shall be visibly identified. 

Unless there is a particular reason, the part used in the subassemblies shall be standard 

and available at the various manufacturers for a duration of 10 years. 

A maintenance note shall be included in the documentation by using the friendly 

explanation with reference to schematic diagrams, drawings or photographs : 

1)  A maintenance schedule and guide providing detailed instructions of 

disassembly, adjustment and calibration of the units, with a list of the tools 

necessary for carrying out these operations. 

2)  A trouble shooting guide listing the main failures for the various systems 

and units. 

 

2.2 Spare 

parts 

 

The contractor shall have responsibility to provide the spare parts required to maintain 

the whole system for a period of 10 years. The contractor shall update the list of spare 

parts in the event of modifications.   

 

The contractor shall draw up a list of mandatory spare parts (due to long lead time, 

redundancy, safety, etc.) and a list of optional spare parts with their failure frequency 

records. 

 

In the case of optional spare parts, the contractor shall categorize the spare parts from 1st 

to 3rd groups depending on their frequencies of malfunction over last 10 years. The 

proposal shall include current purchase prices of the parts and on-site labor charge to 

replace them after the warranty period expires. 

 

2.3 Service 

conditions 

 

Maintenance services shall be provided by the contractor during the equipment lifetime 

at minimum expense. For 5 years after the basic and extended warranties expire, two 

kinds of maintenance service are requested. One is for the regular maintenance and the 

other is for the urgent maintenance during a test period of KARI. 

 

For the regular maintenance, the deadline for action is 2 weeks (for A/S team in Korea, 1 

week) from the reception of the notification of service. For the urgent maintenance, the 

deadline for action is 5 days (for A/S team in Korea, 24 hrs) from the reception of the 


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Space Environment Test Dept. 

notification of service. To meet the deadline of the urgent maintenance service, KARI 

will notify the contractor of the test starting date and the period 2 weeks before the test 

date. According to this, the contractor shall stand by the maintenance crews at the 

contractor's convenient place during the test period(usually 2 weeks).    The number of 

the urgent maintenance service requests is limited to 5 during the entire 5 year 

maintenance period. 

 

The contractor shall include a plan for these requirements in the proposal. The proposal 

shall also include the detailed and total maintenance charges for two kind of maintenance. 

 

The contractor has the responsibility to immediately answer the operational and 

maintenance questions which KARI brings in by FAX or telephone calls until the system 

is dismantled by KARI. General description 

 

 

 

 

 


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Space Environment Test Dept. 

3. Acceptance 

 

3.1 General 

description 

 

The main purpose of the various acceptance tests is to check that the systems and sub-

systems satisfy all the requirements of the present document. Consequently, the 

contractor shall conduct the tests and show the fulfillment of any technical requirements 

of the present document through acceptance tests. To check the fulfillment of the specific 

requirements, KARI can ask the corresponding acceptance tests during the acceptance 

test period. 

 

An acceptance shall also be conducted by the contractor before the delivery for each 

individual piece of equipment in order to check that it meets all its specifications. 

 

All the acceptance procedures shall be written in English, 

Partial check of various elements by the manufacturer, 

Temporary check by the contractor, 

Definitive check by the contractor on the test site in KARI 

 

The contractor shall provide the test procedures in English to KARI or his representative 

for a critical review and approval at least one month before each of the above-mentioned 

acceptance tests. 

 

The final acceptance shall be approved in a written format by KARI or the personnel 

designated by KARI after the contractor successfully carry out the acceptance tests and 

KARI reconfirm them by themselves. 

 

The contractor shall provide all the necessary works, equipment for the installation and 

acceptance test without any additional costs. 

 


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Space Environment Test Dept. 

 

 

 

 

 


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Space Environment Test Dept. 

3.2 Acceptance 

test 

 

3.2.1 

Partial check by the manufacturer 

 

  Amplifier system shall be tested by the manufacturer and certificate before delivery with 

LDS shaker & water cooling system under charge of KARI persons. 

  For the acceptance, the manufacturer should prepare the test procedure and relating the 

detailed configuration & system drawings. 

  Amplifier Characteristics & Harmonic distortion to checked at factory with loading 

conditions. 

  The acceptance material above mentioned should be supplied to KARI 

 

3.2.2 

Definitive test by the contractor on the test site in KARI 

 

This test shall be conducted in two steps: 

hard configuration & connection check 

Overall performance test. 

 

a) Hard configuration 

 

Electrical continuity test on the system 

Amplifier output check 

 

b) Overall performance test 

 

Scope : - verify the complete excitation and measurement system. 

             

For the verification of the overall performance test, KARI will supply the previous test 

results for shaker system (V964). The supply should show that the performance of new 

power amplifier system better than that of previous one. 

 

After the overall performance test, the contractor shall submit the test results in a written 

paper and take the Kari’s approval. 

 

 

 

 


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Space Environment Test Dept. 

6.0 PRELIMINARY 

CHECKS AND PROCEDURES 

 

 

VIBRATOR SERIAL NO. _____1008103/1_________ 

 

 

 PRELIMINARY 

CHECKS 

 

LIMIT 

RESULT 

6.3 

Field diode polarity correct 

 

 

6.4 

Insulation resistance to frame at 500V: 

 

 

 

6.4.1 

Vibrator field coils. 

> 10 Megohms 

 

 

6.4.2 

Degauss coils. 

> 10 Megohms 

 

6.5 Vibrator 

levelled. 

 

 

6.6 

Supply voltage settings checked. 

 

 

6.7 

Calibrate control room monitor settings. 

  100 

Volts 1000 

Amps 

 

 

6.8 

Mercury tilt switch checked for operation. 

 

 

6.9 

CU/FPS water and oil hoses connected to 
vibrator.    CU/FPS filled with water and oil. 

 

 

6.10 

CU/FPS connected to 3 phase mains supply 
and rotation of water and oil pumps checked. 

 

 

6.11 

CU/FPS to Vibrator water and oil hoses 
flushed out, cooling system re-filled with 
distilled water, and oil topped up as necessary.

 

 

6.12 

Remaining equipment, cables, hoses and 
interlocks connected. 

 

 

6.13 

Set: 

Oil pressure to 2500 lbf/in

2.  

 

 

 

Water pressure to 160 lbf/in

2.  

 

  Water 

aeration 

level. 

 

 

6.14 

Water flow interlocks checked. 

 

 

6.15 

Water leak detection checked. 

 

 

6.16 

Oil pressure interlocks checked. 

 

 

6.17 

Raw water supply flow checked. 

 

 

6.18 

Set and record field power supply levels: 

 

 

 

6.18.1 

FPS current (hot) set to 480 amps. 

 

480A 

 

6.18.2 

FPS voltage (hot): Record. 

 

257V 

 

 

 


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Space Environment Test Dept. 

 PRELIMINARY 

CHECKS 

 

LIMIT 

RESULT 

6.19 

Overtemperature interlocks checked. 

 

 

6.20 

All other interlocks checked. 

 

 

6.21 

CU/FPS time delay set to 12 mins. 

 

 

6.22 

Adjust electronic overtravel switch position 
for mid-position of armature travel. 

 

Armature positional datum - top plate to 
armature table: 255.0mm. 

 

 

 

PIC2 Sensor head set to mean position. 

 

 

6.23 

Fit triaxial accelerometers to positions 1,2 
and 3Z.  Fit single axis accelerometers to 
positions 4 and 5. 

 

 

6.24 

Record system noise level at 1Z. 

< 0.2g 

0.04 g 

6.25 Vibrator 

Overtravel switch checked for 

operation. 

 

 

6.26 

Oil and Water systems checked for leaks and 
correct working pressures. 

 

 

 

 

BARE TABLE TESTS 

 

LIMIT 

RESULT 

7.1 

Control at 1Z. 

 

 

 

Displacement 20mm p-p. 

 

 

 

Acceleration level 2g (peak). 

 

 

 

Frequency range 5 to 2500Hz. 

 

 

 

Plot drive signal. 

 

 

 

Plot acceleration at 1,2,3,4 & 5Z. 

 

 

 

Check Accelerometer 1Z waveform 

 

 

7.2 

Armature fundamental resonance: 

1260 - 1390Hz 

1438.7 Hz 

7.3 

Set Bare table Random Test programme for running in 
test with 5 channel extremal control using accelerometers 
at 1,2,3,4 & 5Z. 

 

 

 

Acceleration level  30g (rms). 

 

 

7.4 

Run 10 minutes Random Endurance. 

 

 

7.5 

Plot drive PSD at 0, 5 & 10 minutes. 

 

Plot and record voltage V rms at :  

VIB AMP 

 0 

minutes 

37.2V 23.25V 

 5 

minutes 

37.4V 23.25V 

 10 

minutes 

37.3V 23.3V 

 

Record current A rms at : 

 

 

 0 

minutes 

422. 2A 

743. 5A 


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Space Environment Test Dept. 

 5 

minutes 

422. 2A 

749. 5A 

 10 

minutes 

421. 7A 

746. 5A 

7.6 

Set programme, for Bare Table Sine System Capability 
Check, as stated in System Performance Data Sheet for 
one sweep only with 5 channel extremal control using 
accelerometers at 1,2,3,4 & 5Z. 

 

 

7.7 

Plot distortion at 1Z. 

 

Plot drive signal. 

 

 

 

Plot acceleration at 1,2,3,4,5Z and 1,2,3X &Y. 

 

 

 

Plot    voltage V rms and current A rms. 

 

 

 

Check plots against standards. 

 

 


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Space Environment Test Dept. 

7.0 TESTING 

 

 

VIBRATOR SERIAL NO. _____1008103/1_________ 

 

 

 LOADED 

RANDOM 

TESTS   

LIMIT RESULT 

7.8 

Body suspension and load support systems and pip 
ework checked for leaks. 

 

 

7.9 

PIC 2 Armature position controller set up. 

 

 

7.10 

Fit LDS test load as stated below. (If system 
includes a Head Expander, this can be used in place 
of the test load. Mass and part No. to be recorded.) 

 

 

 

Test load -   

V994 Part No.350550:- 

 

 

 

613 Kg (1351.4 lb) including 
adaptor plate Part No. 380100. 

 

 

7.11 

Shut down aeration. 

 

 

7.12 

  Set programme for Loaded Random Proving Test 
with 5 channel external control using 
accelerometers at 1,2,3,4 & 5Z. 

 

 

 Maximum 

Thrust 

(rms): 

 

See system performance data sheet. Record value 

used. 

 

 

 

Maximum Acceleration level (rms): 

 

See system performance data sheet. Record value 
used. 

 

 

 

7.13 

Plot drive PSD at 0, 5 & 10 minutes. 

 

Record voltage V rms at : 

 

 

 

 0 

minutes 

 

 

 5 

minutes 

 

 

 10 

minutes 

 

 

 

Record current A rms at : 

 

 

 0 

minutes 

 

 

 5 

minutes 

 

 

 10 

minutes 

 

 

7.14 

Remove test load. 

 

 


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Space Environment Test Dept. 

 

 

 

VIBRATOR SERIAL NO. _____1008103/1_________ 

 

 

 

FINAL BARE TABLE SINE TESTS 

 

LIMIT 

RESULT 

7.15 

Repeat 7.1 with vibrator vertical: 

 

 

 

Control at 1Z. 

 

 

 

Displacement 20mm p-p. 

 

 

 

Acceleration level 2g (peak). 

 

 

 

Frequency range 5 to 2500Hz. 

 

 

 

Plot drive signal. 

 

 

 

Plot acceleration at 1,2,3,4 & 5Z. 

 

 

 

Check Accelerometer 1Z waveform 

 

 

7.16 

Armature fundamental resonance: 

1260 - 1390Hz 

 

7.17 No 

action. 

 

 

7.18 

Measure and record: 

 

 

 

Vibrator cooling water pressure. 

 

 

 

Vibrator oil pressure. 

 

 

7.19 

Vibrator stray field measurements at 150mm above 
Armature table using full field setting at operating 
temperature. 

 

 

 

 

 

Position 1 - 28" PCD 

< 2.0 mT 

 

 

 

 

Position 2 - 16" PCD 

< 2.0 mT 

 

 

 

 

Position 3 - Centre 

< 2.0 mT 

 

 

 

 

Position 4 - 16" PCD 

< 2.0 mT 

 

 

 

 

Position 5 - 28" PCD 

< 2.0 mT 

 

7.20 

Project Engineering signature for Special feature 
design validation. 

 

7.21 

Check input supply voltage settings and apply label. 

 

 

 END 

OF 

TESTS 

 

 


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Documentations 

 

The complete system operating and maintenance manuals, including instructions, technical 

specifications, construction drawings and schematics shall be provided with the system upon 

delivery.  

 

Prior to delivery the contractor shall provide complete installation requirements.   

 

All documents shall be written in English or Korean and provided by the contractor in 3 copies and 

electrical file(CD form) on delivery time or at least 1 month before the final acceptance test. 

 

 

 


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IV - 1 

Space Environment Test Dept. 

VII.  Terms and Conditions 

 

Payment Condition 

The payment condition is shown by Table 1. This can be changed by rule of KARI’s 

purchasing office.   

 

Table 1 Payment condition 

 

Payment Stage 

Payment Times 

% of Total 

Initial Payment 

Within EDC + 1 month 

15 

Intermediate 
Payment 

After hardware delivery is completed. 
(LDS site acceptance test is previously completed 
under KARI persons) 

45 

Final Payment 

After KARI site acceptance 

40 


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Space Environment Test Dept. 

VIII.  Format of Proposal 

 

The proposal shall consist of 10 Work Packages (WP). 

 

 

WP 1      : Bidder's Qualification Document 

 

WP 2      : Overview and Technical Proposal 

 

WP 3   : Warranty Proposal 

 

WP 4      : Maintenance Proposal 

 

WP 5   : Training Proposal 

 

WP 6      : Transport - Handling - Storage Proposal 

 

WP 7      : Work Schedule and Installation Plan 

  

WP 8   : Acceptance Test Plan Proposal 

WP 9   : Documentation 

 

WP 10  : Price Proposal 

 

The bidder shall present 6 copies of the proposal. A4 or letter size paper shall be used. The bidder 

is requested to strictly follow the following illustrated format (tabular form). This is very 

important to compare and evaluate different bidders’  proposal. Consequently, disregard for this 

rule may end up with disqualification. Also, well-prepared and well-organized proposal will be 

highly appreciated and evaluated. The landscape orientation will be acceptable for tables. The 

suggested contents in each WP are minimum requirements and works for reminiscences. 

Ambiguous expression will act adversely to the bidder.   

 

Note : The prices which are used in the proposal to calculate the final total and breakdown prices   

            shall be distinguished from the other prices (e.g. optionally suggested parts by the bidder 

            or KARI, . . . ) by marking a.p. (applied price) after the prices. In other words, the sum of   

            a.p. shall be the final total price proposed in the proposal. 

(example) 

Item Price Unit 

Subtotal 

Item #1 

$ 5,000 a.p. 

$ 10,000 

Item #2 

$ 4,000 a.p. 

$ 4,000 

Item #3 

$ 2,000 a.p. 

$ 6,000 

: : : 

  Total 

20,000 

 

 

WP 1 : Bidder's Qualification Document 

 


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Space Environment Test Dept. 

 

The followings shall be included in this WP. 

 

(a) Bidder's last 5 years experience on the prescribed system (“Vibration Control System and Data 

Acquisition and Processing System”) in this "Request for Proposal" including : 

 (1) 

design 

 (2) 

manufacturing 

 

 

(3) installation (specifications, performance, purchaser, supplied year, and price) 

 

(4) training (operation and maintenance) of the facility for foreign countries 

 

(b) Supporting program to maintain high quality of the equipment 

 

(c) Bidder’s Qualification Evidence Documents to show the Part I Section 3.2 and 3.3 in this RFP. 

It may be generated by the ON-SITE Users(can be requested by KARI). The documents include 

personnel's information in charge of the facility, address, FAX number and the others from the 

world well known satellite testing institutes or companies which are using the facilities installed by 

the bidder 

 

(d) Other information 

 1. 

Total 

Employees 

         

- Total number of Employees (Engineer / Technician) 

             

 

- Number of Employees for the directly related area 

   

2. Plant Scale 

         

- Total area of space 

         

- Factory & Building area 

    

3. General brochure 

4. Any documents with which the bidder can show his/her financial and technical 

abilities (e.g. technical awards, bank balance, etc.) 

 

 

WP 2 : Overview and Technical Proposal 

 

Concise and clear expression is required. A long sentence should be broken down into several 

sentences. Detailed block diagrams, figures and photos are recommended for clear illustration. 

 

The bidder should prepare tables for the check list to show the bidder's compliance with the 

"Request for Proposal". The bidder’s compliance list shall be legal bind. This table shall be 


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Space Environment Test Dept. 

located in the front of Overview part. The article numbers in the "Part I. Overview" and "Part II. 

Technical Requirements" in the RFP should be completely enumerated in the table. The table 

format to be followed is as follows: 

 

 

Check List for "Part I. OVERVIEW", "Part II. TECHNICAL REQUIREMENTS", “Part Ⅲ. 

Warranty, Maintenance and other Requirement” and “Part Ⅳ Terms and 

Conditions”(COMPLIANCE LIST

 

ANR 

: Article Number in the Part I and Part II in the RFP 

Y/N 

: Compliance (Yes or No) 

CAP 

: Corresponding Article number in the bidder's Proposal to ANR 

AAM 

: Article number of Added Material in the bidder's proposal which is not mentioned in 

this RFP 

(Exemple) 

 

ANR Y/N 

CAP Remark 

AAM 

Remark 

I-1. yes 

I-1.1 

Ditto 

 

 

I-2. yes 

I-2.1.1 

Ditto 

 

 

I-2.1. yes 

I-2.1.2. 

Ditto 

 

 

…... …… 

…… 

 

 

 

II-1. yes 

II-1.1 

Ditto 

 

 

II-2. yes 

II-2.1.2. 

Ditto 

 

 

II-2.1. yes II-2.1.3. 

Ditto 

 

 

II-2.1.1. 

yes 

II-2.1.5.  The specifications look old. 

We updated them 

 

 

N/A 

N/A 

N/A 

N/A 

II-2.1.4.

We currently developed a 
new method. 

II-2.1.2. yes  II-2.2.1. 

Ditto 

 

 

II-2.1.3. 

no 

II-2.2.2. 

The resolution is high above 
the necessity. 
The current technology for 
the system ............. 
.……... 

 

 

II-2.1.4. yes  II-2.3.1. 

Ditto 

 

 

II-2.1.5. yes  II-2.3.2. 

Ditto 

 

 

II-2.2. 

no 

II-2.3.3. 

This specification is not   
Compatible with II-2.2.2 in 
the Proposal. We suggest 
other Approach. 

 

 

II-2.2.1. yes  II-2.3.4. 

Ditto 

 

 

II-2.2.2. no  II-2.3.5. 

Ditto 

 

 

 

 

WP 3 : Warranty Proposal 

 


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2010. 

 

 
 
Shaker Power Amplifier System 

V - 4 

Space Environment Test Dept. 

3.1. Baseline warranty (2 years) 

 

- plan for the prompt repair 

- information on A/S team   

 

 

WP 4 : Maintenance Proposal 

 

4.1. General description 

 

4.2. Spare parts 

 

 

WP 5 : Training Proposal 

 

5.1. The training program 

 

- contents, location, period, etc. 

 

 

WP 6 : Transport-Handling-Storage Proposal (baseline price) 

 

 

- plan for packaging 

 

- list of special parts and their treatment plan 

 

- storage plan of products for final integration 

- price tables 

 

Note : The abbreviation a.p. shall be marked after the appropriate prices in the tables. 

 

 

WP 7 : Work Schedule and Installation Plan (baseline price) 

 

The work schedule and installation plan shall be shown as in detail as possible in chronological way. 

The installation plan shall be detailed enough to figure out daily progress and include the methods 

and procedures for interface between the equipment and KARI S.I.T.C.(Satellite Integration and 

Test Center)    building (air condition, electricity, treated water, compressed air, etc.). It shall also 

include visits of KARI AITC site. 

 

 

- chronological table for work schedule and installation plan 


background image

  

2010. 

 

 
 
Shaker Power Amplifier System 

V - 5 

Space Environment Test Dept. 

 

- price tables for installation 

 

 

WP 8 : Acceptance Test Plan Proposal 

 

8.1. General description 

 

8.2. Acceptance test   

- schedule 

 

- test list and procedure 

 

8.3. Back-up plan 

For the case that the bidder can not meet the requirements or other contractual binds after the   

contract is awarded, the bidder shall proposed the back-up plan. 

detailed plan and schedule 

 

 

WP 9 : Documentation 

 

9.1. Documentation 

 

- document list (contents, number of page and figure) to be delivered 

   

 

WP 10 : Price Proposal 

 

10.1.Total system price : 

 

All the Price Proposal shall be separately submitted being sealed. 

 

All amounts should be given in U.S. dollars only. 

 

Note :   

The prices which are used in the proposal to calculate the final total and break-down prices shall be 

distinguished from the other prices (e.g. optionally suggested parts by the bidder or KARI, . . . ) by 

marking a.p.(applied price) after the prices. In other words, the sum of a.p. shall be the final total 

price proposed in the proposal. 

The total price is the sum of the break down prices hereafter.