K Class Rocket Motor

Contrail K777-SP

Contrail Rockets
Unknown
Ø 75mm
Total Impulse
1833.0Ns
Burn Time
2.60s
Avg Thrust
695.0N
Max Thrust
1908.0N

Thrust Profile (N)

2.60s Burn Window

Engineered by Contrail Rockets, the K777-SP is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1833.0 Ns over a 2.60 second burn window.

With an average thrust of 695.0 N and a peak of 1908.0 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 75 mm
Length 1016 mm
Hardware 75 40 M SP (2050CC)
Delays (s) P
Specific Impulse 289.7 s
Peak Thrust 1793.08 N
Peak Time T+ 0.112s
T/W Ratio 17.49
Propellant Standard
Profile neutral
Type hybrid
Sparky No

Mass Budget

4050g Total
Casing (Dry)
3405.0g
84.1%
Propellant
645.0g
15.9%
Live Sizing
Flight Envelope

Design wings in your spreadsheet

AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.

Veenie Kit

Need a custom engineering simulator?

The 3D engine on this page is built by Veenie Aerospace. We build bespoke, browser-native digital twins, aerodynamic simulators, and AI physics tools for UAV startups and defense contractors.

Loading calendar...