O Class Rocket Motor

Contrail O6300-BS

Name: Contrail Rockets O6300-BS Rocket Motor
Creator: Veenie Aerospace
License: https://creativecommons.org/licenses/by/4.0/

Contrail Rockets

Unknown

Ø 152mm

Total Impulse

27244.0Ns

Burn Time

4.29s

Avg Thrust

6353.6N

Max Thrust

12732.1N

Thrust Profile (N)

4.29s Burn Window

Engineered by Contrail Rockets, the O6300-BS is a 152mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 27244.0 Ns over a 4.29 second burn window.

With an average thrust of 6353.6 N and a peak of 12732.1 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.

Technical Specifications

Tripoli Rocketry Association, Inc.

Diameter 152 mm

Length 1829 mm

Hardware Single Use

Delays (s) P

Specific Impulse 532.4 s

Peak Thrust 12271 N

Peak Time T+ 0.034s

T/W Ratio 22.66

Propellant Standard

Profile regressive

Type hybrid

Sparky No

Mass Budget

28576g Total

Casing (Dry)

23360.0g

81.7%

Propellant

5216.0g

18.3%

Live Sizing

Flight Envelope

Body Diameter 38 mm

Motor Mount 29 mm

Dry Mass 500 g

Target Apogee 1000 m

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No Curve Data

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