nebula - IARA

NEBULA M42

AVIONICS
NEBULA has a highly reliable, cost effective, double redundant avionics with on board long-range telemetry for communication and live video transmission. It has separate measurement system for sensor data logging. It also has a payload capability of 2-5 Kgs. Which is enough for carrying payloads like CUBESAT and Equipment for Scientific Space experiments.

STAGE II- SOLID

THRUST: 5KN
PROPELLENT: APCP

STAGE I- SOLID

THRUST: 10KN

PROPELLENT: HTPB

RECOVERY
NEBULA has an automated Parachute recovery system for payload and electronics recovery.

Aerodynamics

Aerodynamics plays a vital role in the design of any rocket system and is used for vehicle design evaluation. The two key components are the Nose cone which is made up of fiber glass with reinforced plastic, modeled using the Von-Karmen series to reduce the drag produced in flight and three planform fins are affixed at the bottom to provide stability during flight.

STRUCTURE
The entire rocket Structure is designed by using carbon fiber which has a high strength to weight ratio and is wound to the inner aluminium bulkheads to support the system and distribute the structural, aerodynamic and vibration loads evenly. Rivets are used to connect the ski to the rocket as they are flat and have less skin friction in flight.

NEBULA M42

RECOVERY
NEBULA has an automated Parachute recovery system for payload and electronics recovery.

STAGE II- SOLID

THRUST: 5KN

BURN TIME: 10s

PROPELLENT: APCP

Aerodynamics

Aerodynamics plays a vital role in the design of any rocket system and is used for vehicle design evaluation. The two key components are the Nose cone which is made up of fiber glass with reinforced plastic ,modeled using the Von-karmen series to reduce the drag produced in flight and three planform fins are affixed at the bottom to provide stability during flight.

STAGE I- SOLID

THRUST: 10KN

BURN TIME: 20s

PROPELLENT: HTPB

FLIGHT PROFILE

CHARACTERISTICS

LENGTH:

DIAMETER:

-FIRST STAGE:

-SECOND STAGE:

LIFT-OFF MASS:

DRY-MASS :

PAYLOAD MASS:

OVERALL THRUST:

AVERAGE ISP:

7 m

254 mm

152.4 mm

300 Kgs

150 Kgs

2-5 Kgs

15 KN

180 s

NEBULA M42

NEBULA M42

FLIGHT PROFILE

CHARACTERISTICS

LAUNCH PAD