DEVELOP


POWER GENERATION
PHOTOVOLTAIC
PV
AGRI-PV

Solar photovoltaic (PV) systems convert sunlight directly into electricity using semiconductor materials. PV systems are highly versatile and can be deployed on rooftops, open fields, or integrated into buildings. Solar panels are made of multiple photovoltaic cells, which capture solar energy and convert it into direct current (DC). An inverter then converts DC into alternating current (AC) ready to use from consumers.

Agri-Photovoltaic (Agri-PV) systems combine solar energy generation with agricultural activities, optimizing land use by integrating photovoltaic panels with crop cultivation or livestock farming. These systems are designed to generate renewable energy while providing partial shading that can benefit certain crops, improve water retention in the soil, and reduce heat stress on livestock. Agri-PV solutions are ideal for addressing the dual challenge of sustainable food and energy production. By leveraging higher mounting structures, these systems maintain agricultural productivity while generating clean electricity.

CONVERSION 
20 - 30%
DURABILITY
25 - 30 years

Falcon 9 is a reusable, two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of people and payloads into Earth orbit and beyond. Falcon 9 is the world’s first orbital class reusable rocket. Reusability allows SpaceX to refly the most expensive parts of the rocket, which in turn drives down the cost of space access.

Falcon 9

Overview

HEIGHT
70 m / 229.6 ft
DIAMETER
3.7 m / 12 ft
MASS
549,054 kg / 1,207,920 lb
PAYLOAD TO LEO
22,800 kg / 50,265 lb
PAYLOAD TO GTO
8,300 kg / 18,300 lb
PAYLOAD TO MARS
4,020 kg / 8,860 lb

Falcon 9

First stage

Falcon 9’s first stage incorporates nine Merlin engines and aluminum-lithium alloy tanks containing liquid oxygen and rocket-grade kerosene (RP-1) propellant.Falcon 9 generates more than 1.7 million pounds of thrust at sea level.

The nine Merlin engines on the first stage are gradually throttled near the end of first-stage flight to limit launch vehicle acceleration as the rocket’s mass decreases with the burning of fuel. These engines are also used to reorient the first stage prior to reentry and to decelerate the vehicle for landing.

NUMBER OF ENGINES
9
THRUST AT SEA LEVEL
7,607 kN / 1,710,000 lbf
THRUST IN VACUUM
8,227 kN / 1,849,500 lbf

The Falcon 9 first stage is equipped with four landing legs made of state-of-the-art carbon fiber with aluminum honeycomb.

Placed symmetrically around the base of the rocket, they are stowed at the base of the vehicle and deploy just prior to landing.

Solar Photovoltaic with trackers
Falcon 9 first and second stages after separating in flight
Falcon 9 lifts off with its Iridium-5 payload
Falcon 9 lands on the droneship
Close-up of Falcon 9's Merlin engines during liftoff
Falcon 9 leaves a trail of light as it lifts off from Vandenberg Air Force Base
Falcon 9 lifts off with Dragon for an in-flight test of the Crew Dragon abort system
Falcon 9 lifts off with its Iridium-8 payload
Falcon 9 with its Radarsat payload at sunset before launch
Falcon 9 lands at Cape Canaveral
Falcon 9 vertical with its Iridium payload at moonrise