Attachment D_Final.pdf

ATTACHMENT D

80GSFC25Q7005

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

GODDARD SPACE FLIGHT CENTER

WALLOPS FLIGHT FACILITY

WALLOPS ISLAND, VA 23337

MTM-8 PROCUREMENT SPECIFICATION

FOR

Small Aperture Mobile Telemetry Antenna System

LOCATED

AT

NASA GSFC/WALLOPS FLIGHT FACILITY

WALLOPS ISLAND, VIRGINIA

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MTM-8 Antenna Development TM Modernization Antenna Ground Subsystem Requirements Document (RQMT-000847 Rev-) Medium Aperture (7m) Mobile L/S/C-Band TM Antenna System

2200.01.02.0010 The antenna system shall meet all performance specifications while operating between 1435 and 1525 MHz.

2200.01.02.0015 The antenna system shall meet all performance specifications while operating between 1780 and 1850 MHz.

2200.01.02.0020 The antenna system shall meet all performance specifications while operating between 2200 and 2290 MHz.

2200.01.02.0025 The antenna system shall meet all performance specifications while operating between 2360 and 2395 MHz.

2200.01.02.0030 The antenna system shall meet all performance specifications while operating between 4400 and 4940 MHz.

2200.01.02.0032 The antenna system shall meet all performance specifications while operating between 5091 and 5150 MHz.

2200.01.02.0035 The antenna system shall provide simultaneous RHCP and LHCP receive capability in the L, S and C bands.

2200.01.02.0040 The antenna system shall split the received power of any linear or circular polarized signal into separate RHC and LHC components for signal processing.

2200.01.02.0045 The maximum L-Band axial ratio in RHC and LHC shall be 1.5 dB between 1435 and 1540 MHz.

2200.01.02.0050 The maximum L-Band axial ratio in RHC and LHC shall be 1.5 dB between 1650 and 1710 MHz.

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Requirements Verification Matrix

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2200.01.02.0055 The maximum S-Band axial ratio in RHC and LHC shall be 1.5 dB between 2200 and 2290 MHz.

2200.01.02.0060 The maximum S-Band axial ratio in RHC and LHC shall be 1.5 dB between 2360 and 2395 MHz.

2200.01.02.0065 The maximum C-Band axial ratio in RHC and LHC shall be 1.5 dB between 4400 and 4940 MHz.

2200.01.02.0067 The maximum C-Band axial ratio in RHC and LHC shall be 1.5 dB between 5091 and 5150 MHz.

2200.01.02.0070

The minimum RHC and LHC G/T over the frequency range of 1435 and 1540MHz measured at the output of the multicoupler shall be a minimum of

14.0 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

2200.01.02.0075

The minimum RHC and LHC G/T over the frequency range of 1650 and 1710MHz measured at the output of the multicoupler shall be a minimum of

14.0 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

2200.01.02.0080

The minimum RHC and LHC G/T over the frequency range of 2200 and 2290 MHz measured at the output of the multicoupler shall be a minimum of 17.5 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

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2200.01.02.0085

The minimum RHC and LHC G/T over the frequency range of 2360 and 2395 MHz measured at the multicoupler output shall be a minimum of 17.5 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

2200.01.02.0090

The minimum RHC and LHC G/T over the frequency range of 4400 and 4940 MHz measured at the multicoupler output shall be a minimum of 20.5 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

2200.01.02.0092

The minimum RHC and LHC G/T over the frequency range of 5091 and 5150MHz measured at the multicoupler output shall be a minimum of 20.5 dB/K under the following conditions: 1.) elevation angle greater than 5 deg, 2.) clear sky at ambient temperature.

2200.01.02.0095 The L-Band RHC and LHC receive channels shall have a maximum gain flatness of 1.0 dB pk-pk over any 10 MHz frequency range across the required operating frequency range.

2200.01.02.0100 The S-Band RHC and LHC receive channels shall have a maximum gain flatness of 1.0 dB pk-pk over any 35 MHz frequency range across the required operating frequency range.

2200.01.02.0105 The C-Band RHC and LHC receive channels shall have a maximum gain flatness of 1.5 dB pk-pk over any 400 MHz frequency range across the required operating frequency range.

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2200.01.02.0110 The RF alignment angle between L and S-Band shall be less than 0.2 degrees

2200.01.02.0115 The RF alignment angle between L and C-Band shall be less than 0.1 degrees

2200.01.02.0120 The RF alignment angle between S and C-Band shall be less than 0.1 degrees

2200.01.02.0125 The first sidelobe level shall be ≤ -20 dB referenced from the beam peak at the center of each band.

2200.01.02.0130 The L, S- and C-band Low Noise Amplifiers (LNA) shall have an output 1 dB compression point of no less than +15 dBm over all supported frequency bands.

2200.01.02.0135

The antenna system shall include separate multicouplers for the RHCP and LHCP paths with the performance parameters defined below:

- Frequency: 1435 – 5150 MHz

- 1 input, 12 output

- Gain: 0 to 3 dB

- Noise Factor < 6 dB

- Input Level @ 1 dB Gain Compression: > -10 dBm

- Isolation between outputs: >60 dB

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2200.01.02.0140 The Antenna shall have L-band RHCP and LHCP receive channels with the amplitude balanced to within +/-1.0 dB of each other at the output of the multicoupler.

2200.01.02.0145 The Antenna shall have S-band RHCP and LHCP receive channels with the amplitude balanced to within +/-1.0 dB of each other

2200.01.02.0150 The Antenna shall have C-band RHCP and LHCP receive channels with the amplitude balanced to within +/-1.0 dB of each other

2200.01.02.0155

The Antenna shall be equipped with a filter to reject RFI with the following specifications:

-Passband: 1435-1850MHz, 2200-2400MHz & 4400-5150 MHz -Insertion Loss: 0.5 dB max -Rejection: 40 dB min from 0-1200MHz, 1930-2120 MHz & 2700-4000 MHz

2200.01.02.0160 The antenna system shall provide ability to control the antenna locally at the pededstal

2200.01.02.0165 The Antenna shall disable ACU control when the antenna is being operated at the pedestal.

2200.01.02.0170 The system shall have the following operational modes: Manual, Autotrack, Slave, Search, Program Track, and Launch Acquisition as defined in the

SOW.

2200.01.02.0175 The system shall have touch screen operation that allows access to all modes of operation.

2200.01.02.0180 The system 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.

2200.01.02.0185 The actual antenna AZ and EL position angles and commanded angles shall be displayed with a minimum resolution of 0.01 degree.

Antenna Control Requirements

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2200.01.02.0190 When manual mode is selected, the antenna shall be positioned using hand wheel controls on the ACU front panel or via values typed in via keyboard.

2200.01.02.0195 The antenna hand wheel controls shall be locked-out when operation is in auto or program track modes.

2200.01.02.0200 The autotrack SNR threshold shall have a minimum adjustment of 0.5 dB

2200.01.02.0205 The autotrack threshold hysteresis shall be adjustable from 1 to 20 dB

2200.01.02.0210 The system shall be able to select from up to eight slaving eLTAS sources.

2200.01.02.0215 The system shall display the following for the eLTAS slave sources: table of computed AZ/EL angles based on antenna location, Q and T bit (red or green), SITE ID, latency.

2200.01.02.0220 The system shall have an Ethernet interface that will be used to receive eLTAS data in multicast UDP

2200.01.02.0225 The system shall have the capability to synchronize its clock by selecting either IRIG-B or NTP time

2200.01.02.0235 The system shall have the capability to stow the antenna to preset elevation and azimuth angles.

2200.01.02.0240 The antenna system shall have the capability to remotely engage the stow pin

2200.01.02.0245 The system shall display the brakes & interlock status

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2200.01.02.0250 The antenna system shall have a cable wrap indicator which is displayed

2200.01.02.0255 The antenna system shall sense the cable wrap and when configuring for tracking event, drive the azimuth axis in the direction to reduce, minimize or zero out the cable wrap.

2200.01.02.0257 The antenna system shall display a cable wrap warning after an INP trajectory is loaded if a cable wrap issue during the track is predicted.

2200.01.02.0260 The eLTAS sources shall be selectable in real-time by touch screen or mouse and displayed in a tabular format.

2200.01.02.0262

The antenna system shall capture and record tracking log files for a User Mission Platform support and include the following information at a minimum:

- Date (YYYY-MM-DD, ex. 2024-12-14)

- UTC Time (HH:MM:SS.sss, ex. 00:59:23.111)

- Antenna Location Information (latitude (> 6 decimal places), longitude (> 6 decimal places), WGS-84 ellipsoid height (meters, precision 1 millimeter))

- Selected RX (integer)

- LHC and RHC dB values ( > 2 decimal places)

- LHC and RHC AGC values in volts (> 2 decimal places)

- INP Launch Indicator

- Azimuth and Elevation Commanded/Actual Angles (> 2 decimal places)

- Slave source information (AZ (> 2 decimal places), EL (> 2 decimal places , Q & T Bit , SID (integer) , Latency (milliseconds))

- Time Tagging of each data entry (see UTC specifications above)

- Limit Conditions

- ACU Modes of operation (which mode from the options described in

SOW)

- Demod AZ/EL values and voltages (> 2 decimal places)

- System alarms

2200.01.02.0263 The Antenna shall provide record tracking log files at an adjustable rate between 10 Hz and 100 Hz

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2200.01.02.0264 If system uses hard drive, the system shall be equipped with removable hard drive

2200.01.02.0187 The system shall have a frequency tuning resolution of 10 kHz in all bands of operation.

2200.01.02.0265 The Antenna shall provide L-band Azimuth angle tracking in autotrack to within 0.05 degrees, 1-sigma, with a granularity of 0.01 degrees

2200.01.02.0270 The Antenna shall provide L-band Elevation angle tracking in autotrack to within 0.05 degrees, 1-sigma, with a granularity of 0.01 degrees

2200.01.02.0275 The Antenna shall provide S-band Azimuth angle tracking in autotrack to within 0.05 degrees, 1-sigma, with a granularity of 0.01 degrees

2200.01.02.0280 The Antenna shall provide S-band Elevation angle tracking in autotrack to within 0.05degrees, 1-sigma, with a granularity of 0.01 degrees

2200.01.02.0285 The Antenna shall provide C-band Azimuth angle tracking in autotrack to within 0.05degrees, 1-sigma, with a granularity of 0.001 degrees

2200.01.02.0290 The Antenna shall provide C-band Elevation angle tracking in autotrack to within 0.05degrees, 1-sigma, with a granularity of 0.01 degrees

2200.01.02.0295 The Antenna shall provide Azimuth angle tracking in program track mode to within 0.050 degrees, 1-sigma.

2200.01.02.0300 The Antenna shall provide Elevation tracking in program track mode to within 0.050 degrees, 1-sigma.

2200.01.02.0302 The Antenna shall be configured to track two RF frequencies from any combination of bands.

Antenna Tracking Requirements

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2200.01.02.0303 The Antenna shall switch between L-band autotrack to S-band autotrack when S-band SNR is above the S-band autotracking threshold and when automatic switchover from S-band to L-band autotracking is enabled

2200.01.02.0304 The Antenna shall switch between S-band autotrack to L-band autotrack when L-band SNR is above the L-band autotracking threshold and when automatic switchover from L-band to S-band autotracking is enabled

2200.01.02.0305 The Antenna shall switch between S-band autotrack to C-band autotrack when C-band SNR is above the C-band autotracking threshold and when automatic switchover from C-band to S-band autotracking is enabled

2200.01.02.0310

The Antenna shall switch between C-band autotrack to S-band autotrack when C-band SNR is below the C-band autotracking threshold and when the S-band SNR is above the S-band autotracking threshold and when automatic switchover from C-band to S-band autotracking is enabled.

2200.01.02.0311 The Antenna shall switch between L-band autotrack to C-band autotrack when C-band SNR is above the C-band autotracking threshold and when automatic switchover from C-band to L-band autotracking is enabled

2200.01.02.0312 The Antenna shall switch between C-band autotrack to L-band autotrack when L-band SNR is above the L-band autotracking threshold and when automatic switchover from L-band to C-band autotracking is enabled

2200.01.02.0317 The Antenna shall acquire and maintain autotrack for the primary frequency band once the SNR threshold is met and as long as SNR is at or above the threshold.

2200.01.02.0320 The Antenna shall program track the customer spacecraft with the antenna based on the TLE orbit determination message format as specified in Wallops Range Data Formats (36FC1-TECM-000012).

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2200.01.02.0330 The Antenna shall program track the customer spacecraft with the antenna based on the IIRV orbit determination message format as specified in Wallops Range Data Formats (36FC1-TECM-000012).

2200.01.02.0340 The Antenna shall program track the customer spacecraft with the antenna based on the INPv3 orbit determination message format as specified in Wallops Range Data Formats (36FC1-TECM-000012).

2200.01.02.0345

The antenna system slave mode shall be capable of pointing the antenna based on earth-centered earth-fixed (ECEF) position and velocity data input to the system in the Ethernet Launch Trajectory Acquisition System (eLTAS) data format as specified in Wallops Range Data Formats (36FC1-

TECM-000012).

2200.01.02.0350 The Antenna shall express angular tracking to a resolution of 0.01 degrees.

2200.01.02.0355 The antenna system shall incorporate a test inject capability in the L-Band RHC and LHC receive channels

2200.01.02.0360 The antenna system shall incorporate a test inject capability in the S-Band RHC and LHC receive channels

2200.01.02.0365 The antenna system shall incorporate a test inject capability in the C-Band RHC and LHC receive channels

2200.01.02.0370 The antenna system test inject shall be closed loop and directly coupled or switched into the receive channel prior to the feed Filter/LNA input.

2200.01.02.0380 The test inject shall be one RF line source that feeds each polarization at a balanced RF level not to exceed +/- 1.0dB at the test inject feed point across all bands of operation.

2200.01.02.0385 The antenna system shall include a cable wrap system.

2200.01.02.0405 The antenna sub-system shall have a minimum azimuth travel of +/- 540 degrees over the full azimuth travel range.

2200.01.02.0410 The antenna sub-system shall have total elevation travel greater than or equal to -5 to 185 degrees over the full elevation travel range.

2200.01.02.0415 The Antenna shall have an azimuth velocity that is adjustable and capable of ≥20°/sec

Antenna Pedestal and Drive System Requirements

Test Inject Requirements

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2200.01.02.0420 The Antenna shall have an elevation velocity that is adjustable and capable of ≥ 20°/sec

2200.01.02.0425 The Antenna shall have an azimuth axis acceleration that is adjustable and capable of ≥ 20°/sec^2

2200.01.02.0430 The Antenna shall have an elevation axis acceleration that is adjustable and capable of ≥ 20°/sec^2

2200.01.02.0466 The antenna system shall utilize single mode fiber for all fiber connections.

2200.01.02.0475 The system shall provide a self-contained lightning protection system

2200.01.02.0495 The Antenna shall have electrical disconnects that are in accessible locations.

2200.01.02.0500 The Antenna shall have operating equipment used in the design that does not exceed noise levels of 80 dBA at 3 feet from the equipment. This does not include audible alarms or other warning devices.

2200.01.02.0505 The Antenna shall be designed to protect personnel working at heights from falls in accordance with OSHA 29 CFR 1910/1926 and the ANSI Z359, Fall Protection Code Series.

2200.01.02.0510 The Antenna shall have climbing surfaces both internal and external that are equipped with appropriate non-skid surface or coatings.

Fiber Optic Requirements

Environmental, Safeth & Health Requirements

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2200.01.02.0520

The Antenna shall have interior spaces that are designed with LED lighting meeting the requirements of OSHA 29 CFR 1926.56(a) Table D-3 Illumination and American National Standards Institute (ANSI) A11.1-1965, R1970, Practice for Industrial Lighting, for recommended values of illumination.

2200.01.02.0525 The Antenna shall have interior spaces that are equipped with emergency LED lighting to allow egress in the event of a power loss.

2200.01.02.0530

The Antenna shall have a red color strobe light visible at the antenna to notify any personnel around the antenna that it is under power as defined in Section 4.2.2.3.3 of GSFC-STD-8009 “Goddard Space Flight Center (GSFC) Wallops Flight Facility Range Safety Manual (RSM)”. (Note, this system does not radiate, so a blue light is not required)

2200.01.02.0550

The Antenna shall have position sensing and drive control for limit-stopping to allow for a sufficiently gradual decrease of the antenna angular momentum to prevent the antenna from abruptly hitting the limit-stop and damaging the limit switch or the drive mechanism.

2200.01.02.0555 The Antenna shall have software-controlled limit stops implemented to prevent the antenna from moving beyond its safe operating range on any axis.

2200.01.02.0557 The Antenna shall have electrically controlled limit stops implemented to prevent the antenna from moving beyond its safe operating range on any axis.

2200.01.02.0558 The Antenna shall have hard mechanical stops to prevent the antenna from moving beyond its safe operating range on any axis as a last resort if software or electrical limits fail.

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2200.01.02.0560 The Antenna shall be equipped with emergency stops to disable all moving parts on the antenna system.

2200.01.02.0565 The Antenna shall allow for the expansion of additional emergency stops or interlock devices

2200.01.02.0605 The Antenna shall include a mechanical or electrical release for the brakes in the event electrical power is not available

2200.01.02.0610 The Antenna shall include brake assemblies that are capable of stopping antenna movement when activated.

2200.01.02.0615 The Antenna shall include brake assemblies activate in the event of a power failure (fail-safe)

2200.01.02.0620 The Antenna shall include brake assemblies capable of holding the antenna in wind velocities of 80 miles per hour (mph) without any damage at any antenna position orientation.

2200.01.02.0630 The Antenna shall meet FAA lighting and marking requirements.

2200.01.02.0635 The Antenna shall have all equipment components capable of exceeding 52℃ (125°F) at their surface and should be guarded to prevent inadvertent contact.

2200.01.02.0637 The Antenna shall incorporate a latch on any entry door to secure the door in the position.

2200.01.02.0640 The Antenna shall have isolation devices to isolate hazardous energy sources located outside of any hazardous area for personnel to safely apply LOTO devices prior to beginning maintenance activities.

General Requirements

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2200.01.02.0655 The antenna system shall have a pressurized dry air system to protect critical subassemblies (such as the feed) from moisture, condensation, and corrosion damage.

2200.01.02.0660 The indoor operating components shall operate up to 90% humidity non-condensing

2200.01.02.0665 The indoor operating components shall operate in temperatures from 0 to 50℃ (32 to 122°F)

2200.01.02.0670 The antenna sub-system power shall be 208/120 VAC, 3-phase, 4-wire, 60Hz.

2200.01.02.0675 The antenna shall be equipped with a minimum of four 120-volt 60 Hz AC power outlets in the antenna pedestal.

2200.01.02.0685 The antenna subsystem electrical power distribution (panels, wiring, etc.)

shall be designed and installed in accordance with National Electrical Code.

2200.01.02.0690 The vendor shall provide power transformation component(s) required to allow all antenna system component(s) to interface with voltage(s) and utility line frequency as described in this SRD and corresponding SOW.

2200.01.02.0695 The antenna system vendor shall install 2 spare RF cables in the cable wrap in the pedestal for future use.

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2200.01.02.0700 Any Commercial-Off-The-Shelf (COTS) equipment used in the antenna system will be expected to meet the FCC Class A or B electromagnetic radiated and conducted emission levels.

2200.01.02.0735 The antenna system networked electronics shall accept a Nessus network vulnerability scan without any adverse effect to operational state.

2200.01.02.0740

The antenna system shall meet NASA NPR-7150.2D, NASA Software Engineering Requirements for a Class C non-safety critical system.

Note: Vendor specific requirements/deliverables to meet this requirement are noted in the SOW.

2200.01.02.0745 All Ethernet connected, IP based, subsystem elements shall utilize government furnished network equipment.

2200.01.02.0750 The Antenna shall allow for remote monitor & control of all user-configurable parameters

2200.01.02.0752

The Antenna equipment shall be capable of remote monitor and control and compatible with third party applications by supporting industry standards (i.e., SNMP Read and Write) or by providing an exposed and documented API (i.e., RESTful API) or ICD.

2200.01.02.0754 The Antenna System shall incorporate a dish mounted camera (used for target pointing) with optical zoom that is aligned with the antenna mechanical axis of symmetry.

2200.01.02.0756 The Antenna System dish mounted camera video shall be transmitted to a display viewable by the operator

Monitor & Control Requirements

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2200.01.02.0758 The Antenna system camera lens shall have a minimum optical zoom of 36x.

2200.01.02.0760 The Antenna system camera lens shall have a focal length range of 3.3 mm to 119mm.

2200.01.02.0764 The Antenna system boresight camera shall include an autofocus capability that can be switched on or off by the operator.

2200.01.02.0810 The RMMO TM Antenna Systems shall operate in sustained winds of 40 mph within 3 dB beamwidth of all supported bands without degradation to the pointing accuracy.

2200.01.02.0815 RMMO TM System Antennas shall survive winds of 80 mph winds in any position and 129 mph in stow without structural damage.

2200.01.02.0820 New equipment installed as part of the RMMO TM System that is exposed to outdoor environment shall operate in the ambient temperature range of - 26 C to 54 C (-15° Fahrenheit (F) to +130° F).

2200.01.02.0825

New equipment installed as part of the RMMO TM System, exposed to outdoor environment, in a non-operating state shall withstand continuous exposure to temperatures between -30 C to 70 C (-22° F to +158° F), without solar radiation and with negligible air movement.

Operational Environment Requirements

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2200.01.02.0830 New equipment installed as part of the RMMO TM System, exposed to outdoor environment shall be capable of withstanding rain rates of up to 10 centimeter (cm)/hr (4 in/hr) without structural damage.

2200.01.02.0835 All electrical components, enclosures, cables and connectors exposed to outdoor environment shall be rated for outdoor use and sealed to prevent water intrusion.

2200.01.02.0840 New equipment installed as part of the RMMO TM System, exposed to outdoor environment shall be capable of meeting all performance requirements for up to 100% relative humidity with condensation.

2200.01.02.0845

New equipment installed as part of the RMMO TM System, exposed to outdoor environment shall withstand continuous exposure to relative humidity as low as 5% at an air temperature of 50 C (+122° F) and as high as 100% at temperatures ranging from -30 C to 30 C (-22° F to +86° F), with condensation at all temperatures lower than 30 C (+86° F).

2200.01.02.0850

New equipment installed as part of the RMMO TM System, exposed to outdoor environment shall be capable of meeting all performance requirements in direct solar radiation levels of at least 1,120W/m^2 (355 British Thermal Units (BTU)) per hour (hr) per ft2).

2200.01.02.0855 New equipment installed as part of the RMMO TM System shall be configured to preclude the intrusion of dirt and dust.

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2200.01.02.0860 New equipment installed as part of the RMMO TM System shall be made to prevent infestation by insects, birds and vermin.

2200.01.02.0870 New equipment installed as part of the RMMO TM System shall survive 1-inch diameter hail in winds of 48 km/hr (30 mph) without damage or permanent performance degradation.

2200.01.02.0875 New equipment installed as part of the RMMO TM System shall be capable of withstanding 19mm (0.75 in) of ice in winds of 64 km/hr (40 mph) without damage.

2200.01.02.0880 After coating, the exterior surfaces of both fixed and transportable antenna systems shall be painted with white urethane enamel, matching color chip 27875 or 37875 of FED STD-595.

2200.01.02.0885 The treatment of structural components and joints between dissimilar metals shall follow the guidelines of MIL-STD 889B or approved commercial equivalents.

2200.01.02.0890 Sealant, including mastics, used on joints and seams shall be used according to the sealant manufacturer’s recommendations.

2200.01.02.0905 The antenna system vendor shall provide a complete system FMEA

2200.01.02.0910 The Antenna System shall include spare Line Replaceable Units (LRU) that are required to support the achievement of the required operational availability.

2200.01.02.0915 The Antenna System shall facilitate fault detection and fault isolation to the LRU level.

Availability, Reliability and Maintainability Requirements

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2200.01.02.0920

The Mean Time Between Failure (MTBF) of the antenna system shall be greater than 2,000 hours in accordance with MIL-HDBK-217 or similar method, where the antenna shall be considered as failed when any major antenna component (any LNA, any HPA, Antenna Drive, any RF switch, etc.) fails.

2200.01.02.0925 The Mean Time to Repair (MTTR) for all Range TM System equipment, except for repairs on antennas, shall not exceed 1.0 hours.

2200.01.02.0930 The antenna system shall be designed to meet all the requirements in this document over a life of 20 years with appropriate preventative maintenance and sustainment support.

2200.01.02.0935 Systems and devices shall transport over an IEEE 802 wired Network (Range Mission Network, Corportate Network) for local and remote operations.

2200.01.02.0940 Networked systems and devices shall be IPv4 compatible.

2200.01.02.0945 System network devices shall be IPV6 compatible

2200.01.02.0950 Networked systems that require communication redundancy shall have multiple dedicated {Ethernet} interfaces.

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2200.01.02.0955 Networked systems shall be compatible with standard RJ45 100/1,000/10,000 Copper Ethernet ports.

2200.01.02.0960 Networked systems and devices shall have dedicated unique IPv4/IPv6 address(s).

2200.01.02.0965 Networked systems and devices shall be compatible with DHCP.

2200.01.02.0970 Networked systems and devices shall auto-negotiate speeds {100/1000/10000}.

2200.01.02.0975 Networked systems and devices shall auto-negotiate duplex {Full/Half}.

2200.01.02.0980 Networked systems and devices shall be capable of IEEE standard 802.1X for port-based network access control (PNAC).

2200.01.02.0989 The project shall design the information system with separate user and administrator accounts to support the least privilege principles.

2200.01.02.0990 The information system shall enforce approved authorizations to information and system resources for the defined accounts.

IT Security

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2200.01.02.0992 The information system shall employ least privilege for specific duties allowing users to operate the system to support missions without requiring administrative privileges.

2200.01.02.0993 The information system shall not be purchased with wireless network interfaces, as wireless access is not permitted. (unless specifically required).

2200.01.02.0994 If information systems contain wireless network interfaces, they shall be removed or administratively disabled and secured from re-activation.

2200.01.02.0998

The project shall determine if the information system is capable of auditing the events per the specific operating system configuration specification guide (e.g. Windows 10, Windows Server 2016, Red Hat Enterprise 7, etc.)

documented on the NASA Enterprise Technology Assessments and Digital Standards (ETADS) Office website.

2200.01.02.0999 The project shall implement the audit events the system is capable of per requirement 2200.01.02.0998

2200.01.02.1000 The audit records/log files shall contain information that establishes what type of event occurred. (e.g. user/process identifiers)

2200.01.02.1001 The audit records/log files shall contain information that establishes when the event occurred. (e.g., time stamps)

2200.01.02.1002 The audit records/log files shall contain information that establishes where the event occurred. (e.g., destination addresses, and filenames involved)

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2200.01.02.1003 The audit records/log files shall contain information that establishes the source of the event. (e.g., source addresses and filenames involved)

2200.01.02.1004 The audit records/log files shall contain information that establishes the outcome of the event. (e.g., success/fail indications)

2200.01.02.1005 The 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)

2200.01.02.1006 The project shall allocate audit record/log file capacity that allows for one year’s worth of audit data.

2200.01.02.1007 The system shall use internal system clock(s) to generate time stamps for audit records/log files.

2200.01.02.1008 The system shall record time stamps for audit records that can be mapped to Coordinated Universal Time (UTC) or Greenwich Mean Time (GMT).

2200.01.02.1009

The information system shall compare the internal system clock(s) weekly for systems not connected to a network with access to a recognized time standard with a NASA-controlled time source, such as NISN NTP or an equivalently accurate time service.

2200.01.02.1010

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.

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2200.01.02.1011 The information system shall protect audit information and audit tools from unauthorized access.

2200.01.02.1012 The information system shall protect audit information and audit tools from unauthorized modification.

2200.01.02.1013 The information system shall protect audit information and audit tools from unauthorized deletion.

2200.01.02.1014 The information system shall back up audit records daily onto a physically different system or system component than the system or component being audited.

2200.01.02.1015 The information system shall only authorize the system administrator access to management of audit functionality.

2200.01.02.1016 The information system shall retain audit records/log files for one year to provide support for after-the-fact investigations of security incidents.

2200.01.02.1020 The project shall develop, document and maintain under Configuration Control, a current baseline of the system.

2200.01.02.1021 The project shall document software application configuration settings as part of developing the recovery and reconstitution procedures in connection with the system asset management plan.

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2200.01.02.1022

The project shall document the configuration of the information system operating system (e.g. Windows 10/11, Windows Server 2016/2019/2022, Red Hat Enterprise 8, etc.) as a result of implementing the security configuration specification documented on the NASA Cybersecurity Standard and Engineering Team (CSET) Office website.

2200.01.02.1023

The project shall obtain and install the Agency Security Configuration Standards for the appropriate operating system (e.g. Windows 10/11, Windows Server 2016/2019/2022, Red Hat Enterprise 8, etc.) from the NASA Cybersecurity Standard and Engineering Team (CSET) Office website.

2200.01.02.1024 The project shall configure the information system to provide only essential mission capabilities to the system user account.

2200.01.02.1029 The project shall change/rename the default account name(s) on the system.

2200.01.02.1030 The project shall change the default account password(s) on the system.

2200.01.02.1031

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:

- Upper-case letters

- Lower-case letters

- Numbers

- Special characters.

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2200.01.02.1032 The information system shall enforce a minimum of one character change when new passwords are created.

2200.01.02.1033 The information system shall enforce a 60-day maximum lifetime restriction for passwords.

2200.01.02.1034 The project shall patch all systems to the current level prior to connecting to the network.

2200.01.02.1035 The project shall deliver all systems to the Operational Readiness Review (ORR) with the latest Operating System version installed.

2200.01.02.1036 Application/Operating System maintenance/patching software shall be provided with instructions as outlined in requirements.

2200.01.02.1037 The project shall obtain restoration media with the latest Operating System as delivered to ORR.

2200.01.02.1038 The project shall obtain restoration media with the latest Patch Level as delivered to ORR.

2200.01.02.1039 The project shall obtain restoration media with the latest application version/upgrade as delivered to ORR.

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2200.01.02.1040 The project shall disable all unnecessary ports not specific to functionality on all IP-addressable systems.

2200.01.02.1041 The project shall disable all unnecessary protocols not specific to functionality on all IP-addressable systems

2200.01.02.1042 The system shall be capable of defining and disabling all unnecessary services not specific to functionality on all IP-addressable systems.

2200.01.02.1043

The project shall obtain from the vendor or 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.

2200.01.02.1044

The project shall obtain from the vendor or develop administrator documentation for the information system, system component, or information system service that describes effective use and maintenance of security functions/mechanisms.

2200.01.02.1045

The project shall obtain from the vendor or 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

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2200.01.02.1046

The project shall obtain from the vendor or 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.

2200.01.02.1047

The project shall obtain from the vendor or 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.

2200.01.02.1054 The System shall utilize TLS Versions v1.2 or greater. If not required, all TLS lower versions shall be removed.

2200.01.02.1055 The System shall support the configuration of custom certificates to be used by the Range for (SSL) Connections.

2200.01.02.1056

The System and Vendor Software/Hardware shall be approved under the NASA Covered Article Portfolio (CAP). Sometimes referred to as, NASA Assessed & Cleared products list. If not listed, the system or vendor Software/Hardware shall be submitted to the Agency Covered Article & Technology Supply Chain Assessment Needed (CATSCAN).

2200.01.02.1057

The System shall utilize Software/Hardware that meet the CSET Configuration requirements provided by the either the Range IT Security, Asset Planner, Project Manager or Engineer and based on the Operating System(s) to be delivered.

2200.01.02.1058 The System software shall not use Windows LTSC Licensing.

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2200.01.02.1059 The Vendor shall remediate all vulnerabilities or any severity resulting from a Tenable Nessus scan (utilizing the latest plugins) on all Internet Protocol (IP) addressable systems prior to final acceptance.

2200.01.02.2000 The trailer shall be DOT/FVMSS legal

2200.01.02.2001 The trailer shall have a US STD 5th wheel kingpin hitch

2200.01.02.2002 The kingpin location shall be 36" from the rear face of the Bolster

2200.01.02.2003 The pickup plate thickness shall be 1/4" or greater

2200.01.02.2004 The trailer shall have the ability to be towed by American and European tractors

2200.01.02.2005 The trailer shall have the ability to use both 12 and 24 volt DC input voltage

2200.01.02.2006 The trailer shall have a minimum of two 12,000 lb capacity axles with all-wheel electric disc brakes.

2200.01.02.2007 The trailer shall be a maximum of 8' wide, 41' long, and 39" deck height

2200.01.02.2008 The trailer shall have foldout outriggers capable of supporting the trailer capacity on each which can be pinned in open/closed position.

2200.01.02.2009 The trailer shall have a way to manually retract/extend the outrigger pivot arms in case of drive failure if equipped with an electric or hydraulic system

2200.01.02.2010 If outrigger system is powered, all controls and electrical components shall be installed in a water-resistant enclosure.

2200.01.02.2011 The trailer shall have manually adjustable dual landing tongue jacks

2200.01.02.2012 The trailer shall have all DOT required safety and turn signal lights

2200.01.02.2013 The trailer should have all required European lights and reflectors

2200.01.02.2014 The trailer should have all necessary storage boxes and cases integrated into the structure

2200.01.02.2015 The trailer shall have all required containers and racks for the antenna petals

2200.01.02.2016 The trailer shall have all necessary antenna/feed scaffolding

2200.01.02.2017 The trailer shall be sandblasted, primed with a zinc rich primer, and painted with a white semi-gloss Polyurethane paint.

2200.01.02.2018 The trailer shall have all under carriage seams sealed

Mobile Trailer Requirements

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2200.01.02.2019 The trailer top deck shall be finished in a durable anti-slip material for personnel safety and paint protection.

2200.01.02.2020 The trailer top deck shall be free from any unnecessary obstructions/trip hazards for personnel safety

2200.01.02.2021 Final top deck color to be determined by vendor, but should be a light color

2200.01.02.2022 The trailer shall have a lift mechanism installed to raise/lower the the riser.

This can be electric or hydraulic

2200.01.02.2023 The riser lift mecanism shall have an AC disconnect relay when not in use

2200.01.02.2024 The riser lift mechanism shall have a safety interlock switch for use during antenna assembly/disassembly

2200.01.02.2025 The riser lift mechanism shall have a way to manually raise/lower the riser in case of drive system failure.

2200.01.02.2026 The trailer power input shall be 3 phase 120/208 VAC@60 Hz and utilize a Hubbell connection

2200.01.02.2027 The trailer shall have integrated lift points for shipping overseas

2200.01.02.2028 The trailer should have have any necessary work platforms needed for operators to safely stand and assemble the dish

2200.01.02.2029 The trailer shall have a location designated for grounding/lightning protection purposes

2200.01.02.2030 The trailer should be equipped with stowable access steps or ladders to reach the top deck

2200.01.02.2031 The trailer shall have a flashing indicator or warning light to indicate when the antenna is in operation

2200.01.02.2032 The trailer shall have all appropriate drains/covers to prevent water collection

2200.01.02.2033 The trailer shall be maintainable. All necessary grease zerks, wiring, wear parts, etc must be easily accessable/removable.

2200.01.02.2035 The pedestal levelness shall be within 0.1 degrees measured at the T-head (center of rotation) in any of the quadrants.

2200.01.02.2036 The system should fit into a 40' standard ISO container