Page_14_Item_5__Micro_Fixed_UASs.pdf
PDF 40 KB Posted
- Attached to
- Unmanned Aircraft Systems UAS Federal contract opportunity
- Solicitation number
- D15PS00304
About this file
Amendment 1 Page 14 Replacement
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Questions_and_Answers.pdf | ||
| Sol_D15PS00304_Amd_000003.pdf | ||
| Sol_D15PS00304_Amd_000002.pdf | ||
| Sol_D15PS00304_Amd_000001.pdf | ||
| Pre_Solicitation-Synopsis_D15PS00304.pdf | ||
| Sol_D15PS00304.pdf | ||
| Cover_Letter.pdf | ||
| D15PS00304_1449_UAS_Purchase.pdf |
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Text version
Item 5: Micro Fixed UASs (Type III Fixed), equipped as specified for extended endurance operations.
Flight Performance Specifications
Minimum UAS Requirement Target UAS Requirements (In addition to minimum requirements)
Platform weight under 10 lbs. Platform weight under 8 lbs.
Flight duration of 30 minutes with max payload, standard day.
Flight duration of 4 hours with maximum payload, standard day.
Service ceiling 14,500 feet density altitude. Service ceiling 17,999 feet density altitude.
Maximum sustained wind speed capability of 25 knots. Maximum sustained wind speed capability of 35 knots.
Minimum launch area requirement of 300 feet by 300 feet. Minimum launch area requirement of 100 feet by 100 feet.
Minimum recovery area requirement of 300 feet by 300 feet. Minimum recovery area requirement of 300 feet by 300 feet.
Assisted launch or hand launched or VTOL. Assisted launch method.
Recovery by belly landing. Water recovery.
Noise level of 60 dB at 100 feet (AGL) at full power. Noise level of 50 dB at 100 feet (AGL) at full power.
Operating temperature range of 10–110 degrees Fahrenheit. Operating temperature range of negative 40–110 degrees Fahrenheit.
Environmental criteria of day/night time aircraft lighting (FAR part 91 section 209), water resistant (light rain, snow, mist). Environmental criteria of being water proof.
Surge Flight Speed 45 knots. Surge Flight Speed 50 knots.
Command and Control Specifications
Minimum UAS Requirement Target UAS Requirements (In addition to minimum requirements)
Communication range (RX/TX) C2 of 2 Nautical Miles. Communication range (RX/TX) C2 of 5 Nautical Miles.
Transmit video up to 2 Nautical Miles. Transmit video up to 5 Nautical Miles.
Electric power supply. N/A Uplink control frequency that is a secure digital data link at 900 MHz ISM Band, w/ 256 bit encryption. N/A
Downlink frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, w/ 256 bit encryption
N/A
Programmable Loss of Link (LOL) capability: return to launch and land now.
Loss of Link (LOL): route retrace, land at a specified location.
N/A Aircraft is designed to be interoperable with a medium fixed wing/rotor aircraft, includes; common battery, common GCS and common payloads.
Ground Control Station (GCS) provided and capable of controlling the aircraft offered. N/A
GCS ability to be customized to operate numerous fixed wing and rotor wing platforms with aircraft direct control authority.
GCS is open source with the ability to be customized to operate numerous fixed wing and rotor wing platforms with aircraft direct control authority.
Direct pilot control authority, semi-autonomous flight modes. Flight Operations are geofence restricting operations to G airspace with self-limiting capabilities.
Flight crew required a maximum of 1. N/A Flight planning software must be able to program multiple GPS waypoints with in flight line modifiable options.
Aircraft has the ability to navigate by waypoints at a fixed elevation above the ground based on the terrain.
Ability to record sensor data on-board the aircraft. N/A
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