Enclosure_A_Formatted_Data_Sheet_W31P4Q-26-R-0003.xlsx
XLSX spreadsheet 32 KB Posted
- Attached to
- Request for Information – Small Form Factor Component Technologies for a C-sUAS Interceptor
- Solicitation number
- W31P4Q-26-R-0003
About this file
This Excel file is a detailed technical data sheet for a Request for Information (RFI) related to small form factor component technologies for a C-sUAS Interceptor missile system. The document requests comprehensive specifications for five key missile components: Seeker, Control Actuation System (CAS), Central Processing Unit (CPU), Inertial Measurement Unit (IMU), and Battery. For each component, the data sheet requires detailed technical specifications including technology readiness level (TRL), physical dimensions, performance characteristics, power requirements, and production cost estimates at different volume levels (prototype, moderate purchase, and production).
The RFI is being conducted by the U.S. Army Combat Capabilities Development Command (DEVCOM) Aviation and Missile Center, focusing on research and development of seeker technologies for missile systems in response to evolving Small Unmanned Aircraft Systems (sUAS) threats. The document emphasizes that this is a market research initiative, with responses accepted only from U.S. companies, and no guarantee of contract award. Potential respondents must provide comprehensive technical data across multiple tabs, with submissions limited to Controlled Unclassified Information (CUI) classification. Responses must include specific technical details, production costs in FY25, and manufacturing lead times for each component.
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| File | Type | Posted |
|---|---|---|
| Enclosure_A_Formatted_Data_Sheet_W31P4Q-26-R-0003_Revised_20251215.xlsx | XLSX spreadsheet |
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Instructions
| Instructions: |
| Fill out each tab that you plan to offer in your white paper with the requested specifications. Submissions must have complete information on proposed technology tab to be considered. Ensure specifications are in the units noted. If offering multiple of one component (ex. three seeker options) please duplicate the component tab and rename appopriately. Submissions without this data sheet will not be considered. Items should not be higher classification than CUI and propritary markings will be protected properly. |
Seeker
| Missile Seeker Specifications | Answer | Units |
| Technology Title/Name | ||
| What is the current TRL? | ||
| What type of sensor is your seeker? | RF, IR, SAL, Vis, etc. | |
| What is the Volume required for your seeker? | cm3 | |
| Width | mm | |
| Length | mm | |
| Weight | g | |
| What is the field of regard? | degrees of angle | |
| What is the turn on time? | seconds | |
| What is the minimum detectable feature size? | mrad | |
| What is the effective operating range? | meters | |
| Power Consumption | W | |
| Supply Voltage requirements | V | |
| Missile Seeker Production | Answer | Units |
| How much would the unit cost in a small buy for prototyping? | FY25, $/unit | |
| How much would the unit cost in a moderate purchase (1,000 units) | FY25, $/unit | |
| How much would the unit cost in production level purchase (10,000 units) | FY25, $/unit | |
| How long does it take to produce the seeker? (lead time?) | ||
| What is the current MRL? |
CAS
| Missile Seeker Specifications | Answer | Units |
| Technology Title/Name | ||
| What is the current TRL? | ||
| Mechanical Architecture | Answer | Units |
| Actuation mechanism type | Rotary, Linear, Hybrid, other? | |
| Axis count and configuration | e.g., dual-canard, single-axis pitch | |
| Required volume | cm3 | |
| Total system mass | kg | |
| Maximum achievable control surface deflection angle | deg | |
| Electrical Interface and Command Protocols | Answer | Units |
| Nominal supply voltage range | VDC | |
| Maximum operation current draw, per axis | A | |
| Integrated power driver electronics present | Y/N | |
| Communication/Command protocols supported | e.g., RS-422, custom serial | |
| Control signal type and update rate | e.g., PWM @ XXkHz | |
| Fault handling mechanism | ||
| Performance capability | Answer | Units |
| Stall torque output, per axis | Nm | |
| No-load slew rate | deg/s | |
| Closed-loop frequency response (-3dB point), loaded | Hz | |
| Closed-loop frequency response (-3dB point), unloaded | Hz | |
| Position resolution | arc/min | |
| Encoder type and resolution | ||
| Integration Constraints | Answer | Units |
| Mounting interface geometry (i.e., bolt patter, flange specs, etc) | ||
| Can system be adapted for reduced diameters | Y/N | |
| Module housing or connector architecture | Y/N | |
| Serviceability/LRU considerations | ||
| Qualification Status and Export Controls | Answer | Units |
| Completed qualification testing, including standards | ||
| Missile CAS Production | Answer | Units |
| How much would the unit cost in a small buy for prototyping? | FY25, $/unit | |
| How much would the unit cost in a moderate purchase (1,000 units) | FY25, $/unit | |
| How much would the unit cost in production level purchase (10,000 units) | FY25, $/unit | |
| How long does it take to produce the CAS? (lead time?) | ||
| What is the current MRL? |
CPU
| Missile CPU Specifications | Answer | Units |
| Technology Title/Name | ||
| What is the current TRL? | ||
| What is the packaging volume required for the CPU? | cm3 | |
| Width | mm | |
| Length | mm | |
| Weight | g | |
| How many Processor Cores? | ||
| Volatile Memory | GB | |
| Non-Volatile Memory | GB | |
| I/O | ||
| Operating Temperatures | deg C | |
| Power on time | sec | |
| Power Consumption | W? | |
| Supply Voltage requirements | V? | |
| Missile CPU Production | Answer | Units |
| How much would the unit cost in a small buy for prototyping? | FY25, $/unit | |
| How much would the unit cost in a moderate purchase (1,000 units) | FY25, $/unit | |
| How much would the unit cost in production level purchase (10,000 units) | FY25, $/unit | |
| How long does it take to produce the CPU? (lead time?) | ||
| What is the current MRL? |
IMU
| Missile IMU Package Specifications | Answer | Units |
| Technology Title/Name | ||
| What is the current TRL? | ||
| What is the packaging volume required for the IMU? | cm3 | |
| Width | mm | |
| Length | mm | |
| Weight | g | |
| Power Consumption | W | |
| Supply Voltage requirements | V | |
| Operating temperature | Deg C | |
| Data rate | Hz | |
| Turn on Time | ms | |
| Interface (ie. RS-422) | ||
| Expected Storage Life | years | |
| Temperature Compensation Information | ||
| Gyroscope Specifications | Answer | Units |
| Bias Repeatablility | deg/hr, 1σ | |
| Bias in-run stability | deg/hr, 1σ | |
| Angle Random Walk | deg/√hr | |
| Scale Factor Stability | ppm | |
| Operating range per axis | deg/s | |
| Bandwidth | Hz | |
| What type of gyroscope is it? | MEMS, FOG, or RLG | |
| Accelerometer Specifications | Answer | Units |
| Bias Repeatablility | deg/hr, 1σ | |
| Bias in-run stability | deg/hr, 1σ | |
| Angle Random Walk | deg/√hr | |
| Scale Factor Stability | ppm | |
| Scale Factor Nonlinearity | ppm | |
| Operating range per axis | deg/s | |
| Measurement range | g | |
| Bandwidth | Hz | |
| What type of accelerometer is it? | Piezoresistive or capacitive | |
| Missile IMU Production | Answer | Units |
| How much would the unit cost in a small buy for prototyping? | FY25, $/unit | |
| How much would the unit cost in a moderate purchase (1,000 units) | FY25, $/unit | |
| How much would the unit cost in production level purchase (10,000 units) | FY25, $/unit | |
| How long does it take to produce the IMU? (lead time?) | ||
| What is the current MRL? |
Battery
| Missile Battery Specifications | Answer | Units |
| Technology Title/Name | ||
| What is the current TRL? | ||
| What is the packaging volume required for the battery? | cm3 | |
| Weight | kg | |
| Width | mm | |
| Length | mm | |
| Voltage Range | V | |
| Load | V | |
| Rise Time | sec | |
| Life | sec | |
| Operating Temperature | deg C | |
| Terminal Material | ||
| Shock | g | |
| Vibration | g | |
| Missile IMU Production | Answer | Units |
| How much would the unit cost in a small buy for prototyping? | FY25, $/unit | |
| How much would the unit cost in a moderate purchase (1,000 units) | FY25, $/unit | |
| How much would the unit cost in production level purchase (10,000 units) | FY25, $/unit | |
| How long does it take to produce the IMU? (lead time?) | ||
| What is the current MRL? |
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