Attachment B - RQMT-001107 Required Specifications.xlsx
XLSX spreadsheet 30 KB Posted
- Attached to
- S & C Band Telemetry Antenna System Federal contract opportunity
- Solicitation number
- 80GSFC20Q0006
About this file
This solicitation requests quotes for a S and C Band Telemetry Antenna System to meet the specifications in Attachment B. Quotes are due by the date and time indicated in Block 10 and shall include all shipping and handling costs. The Government will use simplified acquisition procedures defined in FAR 13 to evaluate quotes based on price and other factors specified in the RFQ. A single award will be made from this solicitation. Vendors must quote all items and services listed. The National Aeronautics and Space Administration Goddard Space Center is the contracting agency. Technical acceptability will be determined solely on the content submitted in response to the solicitation as it relates to the minimum required specifications in Attachment B.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SF30.pdf | ||
| Amendment P00001 - Questions and Responses.pdf | ||
| RFQ Clauses.pdf | ||
| Contract Clauses.docx | DOCX document | |
| SF18.pdf | ||
| Attachment A - Statement of Work.pdf |
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Text version
requirements
| ID | Requirement |
| Technical Requirements |
| Technical - Antenna Requirements | |
| 1 | The antenna system shall include the antenna, all necessary control hardware, multicouplers, and tracking receivers for LHC and RHC channels for all supported bands. |
| 2 | The antenna system shall include four tracking receivers. |
| 3 | The antenna system shall include a 12 port multicoupler with unity gain and a channel to channel Isolation of 60dB for each polarization. |
| 4 | The multicoupler shall be full band to cover S-band and downconverted C-band in the frequency range 200 to 2400 MHz. |
| 5 | The antenna system vendor shall install all control room equipment in a standard contractor supplied EIA 19 inch four post rack (H-87” x W-24” x D-30”). |
| 6 | The S-band and C-band Low Noise Amplifiers (LNA) shall have output 1 dB compression point of no less than +15 dBm over all supported frequency bands. |
| 7 | The phase noise induced by the C-band downconverter shall not exceed the following levels: |
-75 dBc/Hz @ 100 Hz, -80 dBc/Hz @ 1 kHz, -85 dBc/Hz @ 10 kHz, -115 dBc/Hz @ 100 kHz, -128 dBc/Hz @ 1 MHz, -130 dBc/Hz @ 10 MHz
| 8 | The antenna system shall provide simultaneous RHCP and LHCP receive capability in the S and C bands. |
| 9 | The antenna system shall split the received power of any linear or circular polarized signal into separate RHC and LHC components for signal processing. |
| 10 | The antenna system shall meet all performance specifications while operating between 2200 and 2290 MHz.(S-band) |
| 11 | The antenna system shall meet all performance specifications while operating between 2360 and 2400 MHz. (S-band) |
| 12 | The antenna system shall meet all performance specifications while operating between 4400 and 5150 MHz. (C-band) |
| 13 | The minimum RHC and LHC G/T over the frequency range of 2200 and 2290MHz measured at the multicoupler output shall be a minimum of 21 dB/K under the following conditions: 1.) elevation angle greater than 10 deg, 2.) clear sky, 3.) Within the operating temperature range. |
| 14 | The minimum RHC and LHC G/T over the frequency range of 2360 and 2400MHz measured at the multicoupler output shall be a minimum of 21 dB/K under the following conditions: 1.) elevation angle greater than 10 deg, 2.) clear sky, 3.) Within the operating temperature range. |
| 15 | The minimum RHC and LHC G/T over the frequency range of 4400 and 5150MHz measured at the multicoupler output shall be a minimum of 24 dB/K under the following conditions: 1.) elevation angle greater than 10 deg, 2.) clear sky, 3.) Within the operating temperature range. |
| 16 | Received C-band signals shall be downconverted as recommended in IRIG-106-19 Section 2.4.7 is |
C-IF Frequency = (5550 MHz − C-RF Frequency) 1150 MHz = (5550 MHz − 4400 MHz) 610 MHz = (5550 MHz − 4940 MHz) 459 MHz = (5550 MHz − 5091 MHz) 400 MHz = (5550 MHz − 5150 MHz)
| 17 | The antenna system shall incorporate a test inject capability in the S-Band RHC and LHC receive channels |
| 18 | The antenna system shall incorporate a test inject capability in the C-Band RHC and LHC receive channels. |
| 19 | The antenna system test inject shall be coupled or switched into the receive channel prior to the Filter/LNA input. |
| 20 | The antenna system test inject shall not impact the system G/T. |
| 21 | The test inject shall be one RF line source that feeds equally both polarizations on the feed. |
| 22 | The maximum S-Band axial ratio in RHC and LHC shall be 1.0 dB between 2200 and 2290 MHz. |
| 23 | The maximum S-Band axial ratio in RHC and LHC shall be 1.0 dB between 2360 and 2400 MHz. |
| 24 | The maximum C-Band axial ratio in RHC and LHC shall be 1.0 dB between 4400 and 5150 MHz. |
| 25 | The S-Band RHC and LHC receive channels shall have a maximum gain flatness of 1.0 dB pk-pk over any 100 MHz frequency range across the required operating frequency range. |
| 26 | The C-Band RHC and LHC receive channels shall have a maximum gain flatness of 1.5 dB pk-pk over any 450 MHz frequency range across the required operating frequency range. |
| 27 | The RF alignment angle between S and C Band shall be less than 0.1 degrees |
| 28 | The vendor shall include pedestal levelness adjustment capability of variable adjustment up to 0.2 degrees |
| 29 | The pedestal levelness shall be within 0.1 degrees measured at the T-head(center of rotation) in any of the quadrants. |
| 30 | The antenna sub-system shall have an outdoor operating temperature of -25 deg to +45 deg C. |
| 31 | The system components shall have an outdoor storage temperature range: -40°C to 55°C. |
| 32 | The indoor operating components shall operate up to 90% humidity non condensing |
| 33 | The indoor operating components shall operate in temperatures from 0 to 50 degrees C |
| 34 | The antenna system shall operate in sustained winds of 40 mph within 3 dB beamwidth of all supported bands without degradation to the pointing accuracy. |
| 35 | The antenna system shall operate in sustained winds of 50 mph with performance degradation to the pointing accuracy (within 3 dB beamwidth of all supported bands). |
| 36 | The antenna system shall survive sustained winds of 129 mph without damage while in the stowed position. |
| 37 | The side lobe levels shall be ≤ -20 dB referenced from the peak at the center of each band and not higher than -17 dB at 80% of all supported bands. |
| 38 | The antenna system shall have a pressurized dry air system to protect critical subassemblies (such as the feed) from moisture, condensation, and corrosion damage. |
| 39 | The center rotation of the elevation T-head shall be at least 28ft above the antenna pad. |
| 40 | The antenna system vendor shall provide end to end RF gain distribution documentation through the receive path. A predicted values shall be provided at PDR and CDR, and final measured values at the Project Closeout Review |
| Technical - Fiber Requirements | |
| 41 | The Government shall provide 9/125 micron single mode fiber to be used for all antenna control and RF signals between the pedestal and control room. |
| 42 | The antenna system vendor shall provide the fiber panel interface used in the antenna and control room rack that uses LC UPC couplers. |
| 43 | The antenna system vendor shall provide any fiber optic requirements outside the GFE fiber standard (such as APC terminations). |
| 44 | All fiber optic requirements shall be met with a minimum cable run length from the antenna to the system tracking rack to be within 1 km. |
| Technical - Camera Requirements | |
| 45 | The system shall incorporate a dish mounted camera (used for target pointing) with optical zoom that is aligned with the antenna mechanical axis of symmetry. |
| 46 | The antenna system shall control the operation of the camera via the ACU or by a camera controller in the same location as the ACU. |
| 47 | The antenna system camera lens shall have a minimum optical zoom of 36x. |
| 48 | The antenna system camera lens shall have a focal length range of 3.3 mm to 119mm. |
| 49 | The antenna system vendor shall provide an HD 19”x10-3/8” monitor that will be integrated into the control room 19 inch four post rack for displaying the camera video in the same location as the ACU. |
| Technical - Lightning Protection System Requirements | |
| 50 | The antenna system shall include a lightning protection system to protect the antenna. |
| 51 | The antenna lightning protection system shall interface with the antenna site's lightning grounding system. |
| 52 | The antenna ground conductors shall be cad welded to the site's ground system. |
| 53 | The antenna system vendor shall provide all required hardware and cables to connect the lightning protection system to the site's lightning ground protection. |
| 54 | The antenna system vendor shall provide the instrument control drawing by the PDR that details the requirements of the lightning protection system and the connections required for the site's lightning ground system. |
| Technical - Antenna Sub-system Requirements | |
| 55 | The antenna system shall provide an electrical hand control as well as manual control for moving the antenna at the pedestal. |
| 56 | When the antenna system is operated at the pedestal the ACU control shall be disabled |
| 57 | All antenna sub-system control electronics shall be enclosed inside the antenna pedestal and under environmental control as required with 100% outdoor humidity and over the operation temperature range. |
| 58 | The antenna sub-system shall have total elevation travel greater than or equal to -5 to 185 degrees over the full Azimuth travel range. |
| 59 | The antenna sub-system shall have hard limits in both axes |
| 60 | The antenna sub-system shall have a minimum azimuth travel of +/- 540 degrees over the full Elevation travel range. |
| 61 | The antenna sub-system velocity shall be at least 10 degrees per second in Elevation. |
| 62 | The antenna sub-system velocity shall be at least 10 degrees per second in Azimuth. |
| 63 | The antenna sub-system acceleration shall be at least 20 degrees per second^2 in elevation. |
| 64 | The antenna sub-system acceleration shall be at least 20 degrees per second^2 in azimuth. |
| 65 | The antenna sub-system power shall be 208/120 VAC, 3-phase, 4-wire, 60Hz. |
| 66 | The antenna system vendor shall install 2 spare RF cables in the cable wrap in the pedestal for future use. |
| 67 | The antenna system pedestal shall have a Safe Mode switch that, when turned on, disables control of the ACU on the antenna. |
| Technical - ACU Requirements | |
| 68 | The ACU shall have the following operational modes: Manual, Autotrack,Slave, Search, Program Track, and Launch Acquisition |
| 69 | All Operational modes shall be selectable from the touch screen control ACU front panel. |
| 70 | The actual antenna AZ and EL position angles and commanded angles shall be displayed on the ACU front panel with a minimum resolution of 0.01 degree. |
| 71 | When manual mode is selected, the antenna shall be positioned using hand wheel controls on the ACU front panel. |
| 72 | The antenna hand wheel controls shall be locked-out when operation is in auto or program track modes. |
| 73 | When manual mode is selected, the antenna shall be capable of being slewed in each axis at a variable rate between 0 and 10 degrees/sec, controlled from the ACU front panel. |
| 74 | The ACU shall provide auto diversity tracking between S and C Band. |
| 75 | When autotrack mode is selected, the antenna shall track and maintain the target within the antenna 3 dB beamwidth when the signal to noise ratio in the receive IF is at least 6 dB (SNR) in the band being tracked. |
| 76 | The autotrack SNR threshold shall have a minimum adjustment of 1 dB from the ACU front panel. |
| 77 | The autotrack threshold hysteresis shall be adjustable from 1 to 20 dB at the ACU front panel. |
| 78 | The launch acquisition mode shall provide a mode from the front panel that is used just after launch to prevent antenna from moving down due to multipath. |
| 79 | The ACU shall synchronize its clock with either IRIG-B time or NTP time. |
| 80 | The time source shall be selectable from the ACU front panel. |
| 81 | The ACU shall have a rate memory capability associated with autotrack mode. |
| 82 | The Rate memory activation shall be selectable from the ACU front panel. |
| 83 | When rate memory is selected, and signal has been lost, the ACU shall automatically switch back to autotrack once the signal is re-acquired. |
| 84 | The rate memory time out period shall be set via the ACU front panel |
| 85 | When search mode is selected, the ACU shall move the antenna in a preselected search pattern. |
| 86 | The ACU search mode patterns shall be raster and spiral. |
| 87 | The search mode pattern and pattern parameters shall be selectable from the ACU front panel. |
| 88 | The search mode shall have a search window width in degrees |
| 89 | The search mode shall have a search window height in degrees |
| 90 | The search mode shall have a search rate in degree/sec |
| 91 | The search mode shall have a search path width in degrees |
| 92 | The program mode shall point the antenna based on information contained in an Internet Prediction (INP), Improved Inter-Range Vector (IIRV), or Two Line Element (TLE) text files. |
| 93 | The type of program track shall be selectable via the front panel |
| 94 | The program mode shall point the antenna according to data contained in an INP(STARRS or INP v3) track file. |
| 95 | The INP(STARRS or INP v3) track file initialization shall be selectable for it to be initialized at a predetermined UTC time entered by the operator. |
| 96 | The INP(STARRS or INP v3) track file initialization shall be selectable for it will be initialized manually by the operator at any specified time. |
| 97 | The program mode shall be capable of pointing the antenna based on a satellite orbit from an IIRV text file. |
| 98 | The program mode shall be capable of pointing the antenna based on a satellite orbit from a TLE text file. |
| 99 | The ACU shall display satellite orbit schedule for every 8 hour period of time based on all active TLEs. |
| 100 | The INP, IIRV, and TLE files shall be transferable to the ACU (accessible from the front) via USB drive. |
| 101 | The slave mode shall be capable of pointing the antenna based on earth-centered earth-fixed (ECEF) position and velocity data input to the ACU in the Ethernet Launch Trajectory Acquisition System (eLTAS) data format. |
| 102 | The ACU shall have an Ethernet interface that will be used to receive eLTAS data in UDP/IP packets. |
| 103 | The ACU shall be able to select from up to eight slaving eLTAS sources. |
| 104 | The eLTAS sources shall be selectable in real-time from the ACU front panel and displayed in a table format. |
| 105 | The ACU shall display the following for the eLTAS slave sources : table of computed AZ/EL angles based on antenna location , Q and T bit good or bad, SITE ID, latency |
| 106 | The run/safe status shall be displayed on the ACU front panel. |
| 107 | The ACU shall have the capability to stow the antenna to preset elevation and azimuth angles. |
| 108 | The ACU shall display the brakes & interlock status. |
| 109 | The ACU shall receive 4 AGC channels from the tracking receivers |
| 110 | The ACU shall receive 4 AM DEMOD signals from the respective tracking receivers |
| 111 | The ACU shall have remote control capabilities. |
| 112 | The antenna system vendor shall provide a software interface document for remote control of the ACU. |
| 113 | The antenna system shall have a remote stow pin which is controlled via the ACU. |
| 114 | The antenna system ACU shall have a cable wrap indicator which is displayed from the front panel. |
| Technical - ACU Data Logging Requirements | |
| 115 | The ACU shall have the capability to log antenna information to a .csv file. |
| 116 | The ACU antenna logging shall be controlled from the ACU front panel for start and stop of all logging. |
| 117 | The rate at which data is logged to file shall be selectable between 1, 5, and 10 Hz. |
| 118 | Log file data samples shall be timestamped with UTC date and time as detailed in the log file data format. |
| 119 | The log file shall contain azimuth and elevation commanded angles as detailed in the log file data format. |
| 120 | The log file shall contain azimuth and elevation actual angles as detailed in the log file data format. |
| 121 | The log file shall contain any limit conditions as detailed in the log file data format. |
| 122 | The log file shall contain the ACU mode as detailed in the log file data format. |
| 123 | The log file shall contain any search mode activated as detailed in the log file data format. |
| 124 | The log file shall contain AGC values for a minimum of 4 tracking receivers as detailed in the log file data format. |
| 125 | The log file shall contain AM DEMOD values for a minimum of 4 receivers as detailed in the log file data format. |
| 126 | The log file shall contain azimuth and elevation angles, data quality bits, time stamp, and source ID from all slave source inputs as detailed in the log file data format. |
| Technical - ACU Automated Testing Requirements | |
| 127 | The ACU shall have built in automated tests. |
| 128 | All ACU automated test parameters shall be entered via the ACU front panel. |
| 129 | The antenna system vendor shall provide details (including pass fail criteria) of each of the ACU automated tests by the Preliminary Design Review (PDR). |
| 130 | The ACU automated tests shall include pass fail criteria and show the pass fail results via the ACU front panel. |
| 131 | The ACU shall execute automated large servo step response tests in azimuth and elevation over the full AZ/EL ranges. |
| 132 | The ACU shall display large servo step response maximum overshoot in seconds and percent. |
| 133 | The ACU shall display large servo step response rise time in seconds for 10 – 90% of travel. |
| 134 | The ACU shall display large step response maximum velocity. |
| 135 | The ACU shall display large step response maximum acceleration. |
| 136 | The ACU shall execute automated small step response tests for discrete movement less than 1 degree in azimuth and elevation. |
| 137 | The ACU shall display small step response maximum overshoot in seconds and percent. |
| 138 | The ACU shall display small step response rise time in seconds for 10 – 90% of travel. |
| 139 | The ACU shall display small step response maximum velocity. |
| 140 | The ACU shall execute a Kv test and display the measured motor back EMF constant Kv. |
| 141 | The ACU shall display the measured velocity used during the Kv test. |
| 142 | The ACU shall execute a Ka test that displays the servo amplifier gain constant Ka. |
| 143 | The ACU shall display the measured acceleration used during the Ka test. |
| 144 | The ACU shall execute an error gradient test in azimuth . |
| 145 | The ACU shall execute an error gradient test in elevation. |
| 146 |
The ACU error gradient test angle offset shall be user defined.
| 147 | The ACU shall execute an automated G/T measurement in both polarizations and all supported bands. |
| 148 | The ACU shall have the capability to output test results from any automated test to an Adobe PDF file. |
| 149 | The PDF files shall be time stamped with date and time when the test was completed. |
| Condition Based Monitoring Requirements | |
| 150 | The antenna system shall contain monitoring that is viewable from the ACU front panel. |
| 151 | The antenna system T-Head and feed sensors shall include Temperature, humidity, and moisture monitoring from the ACU front panel. |
| 152 | The antenna system monitors shall include air compressor and line pressure monitoring from the ACU front panel. |
| 153 | The antenna system monitors shall include vibration sensor monitoring from the ACU front panel. |
| 154 | The antenna system monitors shall include line power sensor monitoring from the ACU front panel. |
| 155 | The antenna system monitors shall include simple ON/OFF sensor monitoring from the ACU front panel. |
| IT Requirements | |
| 156 | All systems shall pass an Information Technology Security Vulnerability Assessment. |
| 157 | The ACU shall use sustainable operating system such as longterm Windows or RHEL 8. |
| 158 | The antenna system vendor shall provide an operating system sustainability plan for a minimum of 10 years after delivery of the system. |
| 159 | The system shall not utilize wireless network interfaces. |
| 160 | The vendor shall implement OS Security Configuration features specified by the NASA Enterprise Technology Assessments and Digital Standards (ETADS) Office. The ETADS features include a combination of Defense Information Systems Agency (DISA) Security Technical Implementation Guide (STIG) and Center for Internet Security (CIS) guidance. Security configuration guidelines for the following operating systems will be provided upon request: |
Apple macOS 10.15 Apple macOS 10.14 Red Hat Enterprise Linux 8 Red Hat Enterprise Linux 7 Red Hat Enterprise Linux 6 Windows 10 Windows Server 2019 Windows Server 2016 Windows Server 2012 Windows Server 2008 R2
| 161 | The vendor shall implement event auditing that is provided by the OS used on any information system per requirement 160. |
| 162 | Audit records/log files shall contain information that establishes what type of event occurred. (e.g. user/process identifiers) |
| 163 | Audit records/log files shall contain information that establishes when the event occurred. (e.g time stamps) |
| 164 | Audit records/log files shall contain information that establishes where the event occurred. (e.g. destination addresses and filenames involved) |
| 165 | Audit records/log files shall contain information that establishes the source of the event. (e.g. source addresses and filenames involved) |
| 166 | Audit records/log files shall contain information that establishes the outcome of the event. (e.g. success/fail indications) |
| 167 | Audit records/log files shall contain information that establishes the identity of any individuals or subjects associated with the event. (e.g. access control or flow control rules invoked) |
| 168 | The information system shall allocate audit record/log file capacity that allows for one year’s worth of audit data. |
| 169 | The information system shall use internal system clock(s) to generate time stamps for audit records/log files. |
| 170 | The information system shall record time stamps for audit records that can be mapped to Coordinated Universal Time (UTC) or Greenwich Mean Time (GMT). |
| 171 | The information system shall generate audit time stamps based on the internal system clock that is synchronized to NTP when NTP is available. If NTP is not available, then a method to manually set the internal system clock shall be provided. |
| 172 | The information system shall synchronize the internal system clock(s) to the authoritative time source when the time difference is greater than 60 seconds to ensure adequate support for mission and forensic requirements. |
| 173 | The information system shall protect audit information and audit tools from unauthorized access. |
| 174 | The information system shall protect audit information and audit tools from unauthorized modification. |
| 175 | The information system shall protect audit information and audit tools from unauthorized deletion. |
| 176 | The information system shall have the capability to back up audit records daily onto a physically different system that is network accessible. |
| 177 | The information system shall only authorize the system administrator access to management of audit functionality. |
| 178 | The information system shall retain audit records/log files for one year to provide support for after-the-fact investigations of security incidents. |
| 179 | In order to restore the information system in the event of data or file corruption, the vendor shall provide documentation including procedures and configuration settings to restore all software applications used for operation. |
| 180 | The vendor shall document OS Security Configuration features as a result of implementing specifications provided by the NASA Enterprise Technology Assessments and Digital Standards (ETADS) Office. The ETADS features include a combination of Defense Information Systems Agency (DISA) Security Technical Implementation Guide (STIG) and Center for Internet Security (CIS) guidance. Security configuration guidelines for the following operating systems will be provided upon request: |
Apple macOS 10.15 Apple macOS 10.14 Red Hat Enterprise Linux 8 Red Hat Enterprise Linux 7 Red Hat Enterprise Linux 6 Windows 10 Windows Server 2019 Windows Server 2016 Windows Server 2012 Windows Server 2008 R2
| 181 | The vendor shall configure the information system to provide only essential mission capabilities to the system user account. |
| 182 | The system shall provide a means to change/rename default account names. |
| 183 | The system shall provide a means to change default account passwords. |
| 184 | The system shall enforce NASA’s minimum password complexity requirements which include the following: |
1) Use of at least 12 characters
2) Include 3 of the 4 character types:
a) Upper-case letters
b) Lower-case letters
c) Numbers
d) Special characters
| 185 | The information system shall enforce a minimum of one character change when new passwords are created. |
| 186 | The information system shall enforce a 60-day maximum lifetime restriction for passwords. |
| 187 | The vendor shall patch all systems to the most current level prior to installation at Wallops. |
| 188 | The vendor shall provide procedures/instructions for installing operating system or application software updates that would be distributed by the vendor after the delivery, as part of any warranty or maintenance included with the contract. |
| 189 | The vendor shall provide restoration media with the latest Operating System as delivered. |
| 190 | The vendor shall provide operating system restoration media with the latest Patch Level as delivered with the system. |
| 191 | The vendor shall provide application restoration media with the latest application version/upgrade as delivered with the system. |
| 192 | The vendor shall disable all unnecessary ports not specific to functionality on all IP-addressable systems. |
| 193 | The vendor shall disable all unnecessary protocols not specific to functionality on all IP-addressable systems. |
| 194 | The vendor shall disable all unnecessary services not specific to functionality on all IP-addressable systems. |
| 195 | The vendor shall develop administrator documentation for the information system, system component, or information system service that describes secure configuration, installation, and operation of the system, component, or service. |
| 196 | The vendor shall develop administrator documentation for the information system, system component, or information system service that describes effective use and maintenance of security functions/mechanisms. |
| 197 | The vendor shall develop user documentation for the information system, system component, or information system service that describes user- accessible security functions/mechanisms and how to effectively use the security functions/mechanism. |
| 198 | The vendor shall develop user documentation for the information system, system component, or information system service that describes methods for user interaction, which enables individuals to use the system, component, or service in a more secure manner. |
| 199 | The vendor shall develop user documentation for the information system, system component, or information system service that describes user responsibilities in maintaining the security of the system, component, or service. |
| 200 | All information system devices shall utilize Anti-Virus Software. |
| 201 | Anti-Virus Software shall be installed and running for FAT. |
| Review Requirements | |
| 202 | The antenna system vendor shall support the following lifecycle reviews: PDR, CDR, TRR for FAT, TRR for SAT, Pre-ship review, and the Project Closeout review. |
| 203 | The antenna system vendor design package shall include the component level analysis showing the system's ability to achieve the required tracking accuracy requirements at the PDR, & CDR. |
| 204 | The antenna system vendor design package shall include detailed block diagrams, flow chart level descriptions, electronics and pedestal layouts, software description, and operator interfaces at the PDR, CDR, and Project Closeout Review. |
| 205 | The antenna system vendor shall provide the interface control drawing no later than 8 weeks after contract start that details the requirements of the pad and bolt circle required to meet tracking accuracy requirements. |
| 206 | The antenna system vendor shall support the factory(at vendor's site) and site acceptance testing at Wallops and deliver test results by 15 days following the test completion with the Government's concurrence. |
| 207 | The antenna system vendor shall generate and deliver the factory and site acceptance testing procedures to the Government for review at least 60 calendar days prior to the start of testing. |
| 208 | The antenna system vendor shall perform the following RF testing on a calibrated Range: Antenna pattern, RF alignment, and tracking accuracy shall be measured on a calibrated range. |
| 209 | The antenna system vendor shall provide hard and soft copies of all technical data including specifications, interface data, system and interconnect drawings, technical and vendor manuals, user guides, training materials, and maintenance procedures. |
| Quality Requirements | |
| 210 | Labeling of hardware shall be legible and clearly visible. |
| 211 | The antenna system vendor shall provide the workmanship standards used for cabling, crimping, harnessing, and wiring. |
| 212 | The antenna system vendor shall provide an overview of their quality assurance program. |
| 213 | Tie wraps or lacing shall be used as required to secure cabling in place. |
| Maintainability Requirements | |
| 214 | The antenna system vendor shall provide a system FMEA with any supporting documents and analysis at the PDR, and CDR. |
| 215 | The antenna system vendor shall provide training for antenna operation and maintenance for minimum of 10 personnel at Wallops Flight Facility after the SAT. |
| 216 | The antenna system vendor shall provide maintenance procedures with delivery of the antenna. |
| 217 | The antenna system vendor shall provide a recommended critical spares list which includes an itemized cost for each item in the proposal by the PDR, CDR, and the Project Closeout Review. |
| Sustainability Requirements | |
| 218 | The antenna system vendor shall provide software patches on a minimum of a quarterly basis(if available). |
| 219 | The antenna system vendor shall provide emergency software patches if necessary. |
| Reliability Requirements | |
| 220 | MTBF for the system shall be at least 6000 hours assuming 100% duty cycle starting after completed site acceptance testing. |
| 221 | MTTR shall be less than 2 hours |
| Availability Requirements | |
| 222 | The antenna system shall provide an inherent availability (Ai) of at least 99.95% |
| Safety Requirements | |
| 223 | The antenna system vendor shall provide their electrostatic discharge control plan. |
| 224 | The antenna system vendor shall include provisions for fall protection such as anchor points. |
| 225 | The antenna system shall have a visual indicator light for active servos. |
| Human Factors Requirements | |
| 226 | The ACU shall utilize a touchscreen for operator control. The touchscreen shall not require a stylus pen. |
| 227 | The ACU shall have a keyboard that can be used to enter parameter values and mouse that can be used to provide the same functions as the touch screen. |
| Lifecycle Management Requirements | |
| 228 | The project shall include extended warranties as priced options in the vendor proposal for the purchased equipment |
| 229 | The antenna system vendor shall provide warranty information |
| 230 | The antenna system vendor shall provide service agreement information (if applicable) as priced options in the vendor proposal. |
| 231 | Vendor shall provide all applicable system manuals, equipment specifications, ID numbers (such as part number, model number, other unique identifiers), and a full bill of materials. |
RQMT-001107, REV A
NASA Wallops Flight Facility S & C Band Telemetry Antenna System Requirements
File details come from the government source that posted it. Updated .