M Class Rocket Motor

Contrail M2700-BS

Name: Contrail Rockets M2700-BS Rocket Motor
Creator: Veenie Aerospace
License: https://creativecommons.org/licenses/by/4.0/

Contrail Rockets

Unknown

Ø 98mm

Total Impulse

6034.0Ns

Burn Time

2.30s

Avg Thrust

2644.8N

Max Thrust

5483.6N

Thrust Profile (N)

2.30s Burn Window

Engineered by Contrail Rockets, the M2700-BS is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 6034.0 Ns over a 2.30 second burn window.

With an average thrust of 2644.8 N and a peak of 5483.6 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.

Technical Specifications

Tripoli Rocketry Association, Inc.

Diameter 98 mm

Length 1524 mm

Hardware Single Use

Delays (s) P

Specific Impulse 355.5 s

Peak Thrust 6442.25 N

Peak Time T+ 0.504s

T/W Ratio 25.84

Propellant Standard

Profile dual-peak

Type hybrid

Sparky No

Mass Budget

10432g Total

Casing (Dry)

8702.0g

83.4%

Propellant

1730.0g

16.6%

Live Sizing

Flight Envelope

Body Diameter 38 mm

Motor Mount 29 mm

Dry Mass 500 g

Target Apogee 1000 m

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Comparable M-Class Alternatives

5342M1560-P

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