HARDWARE / PRODUCTUpdated 24 Jul 2026

FPPT — Fiber-Fed Pulsed Plasma Thruster

CU Aerospace
FPPT — Fiber-Fed Pulsed Plasma Thruster

CU Aerospace’s Fiber-Fed Pulsed Plasma Thruster (FPPT) provides very high specific impulse greater than 3,500 seconds via a 10-microsecond electromagnetic pulse discharge using solid PTFE (Teflon®) fiber propellant spooled inside the package. No pressurized propellant tank or valving that can leak propellant is required, making FPPT inherently safe and compliant with range safety regulations. The […]

Key figurescomparable across the catalogue

Thrust
5 N
Specific impulse
3,500 s
Total impulse
25,000 N·s
Lead time
9 months

Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.

As published by the supplier

Thruster type
Pulsed plasma thruster (PPT) with electromagnetic thrust vectoring
Specific impulse (Isp)
>3,500 s
Total impulse (1.7L package)
>25,000 N-s
Total impulse range
1,000–600,000 N-s (0.7L–53L)
Package size range
0.7 L to 53 L (1U to ESPA-class)
Propellant
PTFE (Teflon®) fiber; solid, inert, no pressure vessel required
Thrust vectoring
±5° pitch and yaw electromagnetic steering
Pulse duration
10 microseconds
Lead time (standard 1.7U)
<9 months dual fault tolerant unit

About

CU Aerospace’s Fiber-Fed Pulsed Plasma Thruster (FPPT) provides very high specific impulse greater than 3,500 seconds via a 10-microsecond electromagnetic pulse discharge using solid PTFE (Teflon®) fiber propellant spooled inside the package. No pressurized propellant tank or valving that can leak propellant is required, making FPPT inherently safe and compliant with range safety regulations. The system includes electromagnetic thrust vectoring of approximately ±5 degrees in pitch and yaw. FPPT delivers total impulse greater than 25,000 N-s in a 1.7-liter package and has evolved into form factors from 0.7 L to 53 L providing total impulses from 1,000 to 600,000 N-s. Applications include orbit raising and lowering, inclination change, collision avoidance, drag makeup, deorbiting, and deep space missions. The ESPA-class FPPT variant can serve as the propulsion system for active debris removal (ADR) satellites. Isp and total impulse are competitive with Hall and ion thrusters at significantly lower cost.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.cuaerospace.com ↗

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