December 28, 2025
Description
Payload Rocket – Standard Size Engine V2 is a modular hobbyist rocket featuring a two-layer body design for improved stability and engine flexibility. The inner engine mount is 22 mm in diameter, while the outer body is 33 mm, allowing secure mounting of A, B, and C class 18 mm motors. Standing 161.91 mm tall with a fin span of 129.98 mm, this rocket can carry a payload of up to 13.4986 cm³.
Its clamshell-style nose cone splits open mid-flight to release payloads such as streamers, sensors, or small electronics. Built for stable flights and easy recovery, V2 is ideal for educational projects, backyard launches, and payload testing. Its dual-layer design ensures durability and consistent performance.
Launch with an A motor for low-altitude testing, a B motor for mid-range flights, or a C motor for dramatic maximum-altitude flights.
Launch location: Argyle, MS, Maryland. The Payload Rocket Standard Size Engine V2 combines innovation, reliability, and fun, making it perfect for hobbyists and STEM projects alike.
Here are some extra things you can do for fun:
1️⃣ Launch Card – Payload Rocket Standard Size Engine V2
Rocket Name: Payload Rocket – Standard Size Engine V2
Manufacturer: [Your Name / Brand]
Motor Compatibility: A, B, C class motors (18 mm inner mount)
Launch Date: [Insert Date]
Location: [Insert Location]
Rocket Dimensions:
Key Features:
Recommended Launch Setup:
Safety Notes:
Flight Plan:
| Specification | Details |
|---|---|
| Rocket Name | Payload Rocket – Standard Size Engine V2 |
| Engine Type | A, B, C class (18 mm inner mount) |
| Length | 161.91 mm |
| Inner Engine Mount Diameter | 22 mm |
| Outer Body Diameter | 33 mm |
| Fin Type | Triangular, attached to outer body |
| Fin Span | 129.98 mm |
| Maximum Payload Volume | 13.4986 cm³ |
| Nose Cone Type | Split-clamshell, deployable payload |
| Construction Material | PLA / lightweight hobby-grade material |
| Recommended Launch Rod | 36–48 inches |
| Recovery System | Streamer / small parachute |
| Max Altitude | A ~50–60 ft, B ~120–150 ft, C ~200+ ft (approx.) |
| Flight Description | Vertical lift-off, mid-air payload deployment, stable descent |
License:
BY-NC-ND