Using Radiant Turn Coordinators on 28 V Aircraft Electrical Systems
- James Wiebe
- 48 minutes ago
- 3 min read
Radiant Technical Note 11.6.2025
Using Radiant Turn Coordinators on 28 V Aircraft Electrical Systems
(Not applicable to SafeTurn portable units)
Applies to: Radiant Turn Coordinator products, when operated from 24–28 V class aircraft electrical systems (“28 V” systems).
Does not apply to: Radiant SafeTurn portable units (self-powered; do not add this resistor).
1. Background
Radiant Turn Coordinators use a robust linear power chain:
External Bus → 9.5 V Pre-Regulator → 5.0 V Regulator → Li-Ion Charger → Li-Ion Pack → Internal Loads
The internal pre-regulator is rated to 30 V (with high transient tolerance), and downstream devices are selected for harsh environments. Electrically, these units can be tied to many aircraft buses.
However, a “28 V” aircraft system normally operates:
In flight: about 27.5–28.5 V
With real-world variation and hot regulators near the top of that range
Feeding a 9.5 V linear pre-regulator directly from this range at charging current forces it to burn significant power as heat. That’s survivable but unnecessary—and over time, unwanted.
Radiant’s design supports a simple external addition that:
Reduces internal thermal stress
Improves reliability margin
Requires no changes inside the Radiant Turn Coordinator
2. Recommended Solution for 28 V Systems
For experimental aircraft with 24–28 V systems, Radiant recommends adding a single external series resistor in the power feed the Radiant Turn Coordinator.
Use a 100 Ω, 5 W (or higher) resistor in series with the +28 V supply line feeding the unit.
Radiant does not supply this resistor; it is a standard, easily sourced component.
How it works (conceptual)
At a configured internal load/charge of about 160 mA, the resistor drops part of the voltage before the 9.5 V pre-regulator.
The external resistor now dissipates a significant portion of the waste heat instead of the pre-regulator IC.
The pre-regulator runs cooler while maintaining proper operation over the typical 28 V range.
Example (worst nominal: 28.5 V bus)
Assumptions:
Bus: 28.5 V
R_EXT: 100 Ω
I: 0.16 A
Pre-reg target: 9.5 V
Then:
Drop across R_EXT:VR=0.16×100=16.0 V
Pre-reg input: Vpre-in=28.5−16.0=12.5 V
Pre-reg dissipation: Ppre=(12.5−9.5)×0.16=0.48 W
Resistor dissipation: PR=0.162×100=2.56 W
Conclusion: the resistor (properly rated) runs warm and happy; the pre-regulator is kept in a comfortable power range instead of being pushed hard.
At typical in-flight voltages (27.5–28.0 V), numbers improve slightly further.
3. Behavior at Lower / Abnormal Voltages
This recommendation targets normal 28 V operation and thermal robustness:
At 27.5–28.5 V (normal regulated):
Full functionality
Good thermal margin on internal regulators
At lower bus voltages (e.g. 24–26 V, weak bus / alternator offline):
The series resistor reduces headroom; charge current may taper or stop.
This is expected and acceptable for abnormal conditions.
At brief higher inputs within device ratings:
The series resistor further limits stress on the pre-regulator.
Installers should treat this as good practice for experimental 28 V aircraft, not as certified data.
4. Installation Guidance (Experimental Use)
Basic wiring:
Aircraft 24–28 V bus → appropriate breaker or fuse
Breaker/fuse output → 100 Ω, ≥5 W series resistor
Resistor output → Turn Coordinator +V input
Turn Coordinator ground → aircraft ground
Notes:
Mount the resistor so it has airflow and is mechanically secure.
Keep it clear of plastics and harnesses sensitive to elevated temperature.
Use aviation-appropriate wiring, terminations, and strain relief.
Verify operation at your aircraft’s actual bus voltages after installation.
5. Example Orderable Part (Installer Convenience)
Radiant does not supply the resistor. A typical suitable example:
100 Ω, 5 W flameproof or wirewound resistor, axial or chassis mount
Example (one of many acceptable choices): a 5 W, 100 Ω wirewound resistor from a major brand via Digi-Key / Mouser / equivalent.
Any equivalent 100 Ω, ≥5 W resistor from a reputable manufacturer, installed correctly, is acceptable.
6. Scope Clarification
This recommendation supports and applies to:
Radiant SafePanel (experimental installations)
Radiant RTCC (experimental installations)
️ This recommendation does not apply to:
SafeTurn portable units
Certified aircraft or TSO/STC applications (this is not approved data)



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