|
Tronador LSA |
Comision Nacional de Actividades Espaciales (CONAE) * Vehiculos space Nueva Generation (VENG)
Argentina has two orbital LV projects.
One is the hypergolic project form the civil space agency, CONAE, commonly
known as the TRONADOR Project, or more correctly ISCUL (Inyector Satelital
de Cargas Utiles y Livianas, or Satellite Injector of Useful and Light Payloads).
The second project is from the Ministry of Defense, it has a project to develop
a "big" solid rocket AGUILA.
Tronador-III LSA
CONAE revealed
in 2015 that the new Tronador III would be a vehicle with 2 stages, a height
of 35 meters, a diameter of 2.5 meters and a weight of 89 tons at the time of
takeoff, with the ability to payload weight of up to 1000 kg for a LEO orbit
between 400 and 600 km altitude.
The state-owned company YPF Technology (Y-TEC) is responsible for the development of the fuel used in the first stage of the launcher. Tronador III has two tanks of aluminum structure that can hold 34,000 liters of fuel and 45,000 liquid oxygen. The four engines produce enough power to bring the rocket to a height of 100 km in just 3 minutes.
Seconds after disconnecting the first stage, the upper stage ignited. It is powered by a single engine with 3 tons of thrust. Unlike the first-stage engines, the single engine uses monomethyl-hydrazine (MMH) and dinitrogen tetroxide (NTO) and consumes 8 liters per second. Its function is to lift the payload to a height of more than 400 km in order to finally transport it into orbit.
History
2021, November
-- Within the framework of the reactivation of strategic projects, the Ministry
of Science, Technology and Innovation of the Nation (MINCyT) relaunched the
"Access to Space" program carried out by the National Commission for Space Activities
(CONAE), which includes the development of vehicles experimental VExs and Tronador
II/III launchers, as well as associated auxiliary infrastructure and launch
bases. There is a planned investment of about 4,500 million pesos in 2022. |
|
2017, April 21 - On this
day (local April 20) the launch of the VEX-5A was stopped after 8 seconds
during the successful flight, because the fuel supply was abruptly interrupted.
The rocket was fall back and explodes on ground. It is reported that the filling
consisted of: 1730kg of liquid oxygen, 994kg of kerosene, 50kg of monomethylhydrazine
and 95kg of nitric acid. This would mean that the VEX-5A was a two-stage vehicle.
2016, Nov. 22 -
The VEX 5-A rocket test was suspended today for "technical" reasons only
a few minutes before launch from the Punta Indio space base, the National Space
Activities Commission reported.
Apparently it was not possible to activate
a valve of the pressure system a few minutes before the launch.
2016, Nov. 21 - In the
absence of climatic inconveniences in the Samborombón Bay area, the launch of the
VEX-5A Experimental Vehicle is scheduled to take place between 22 and 24
November.
The VEX-5A
is little more than 18 meters high, 1.5
meters in diameter with an
engine power of 11 tons. It weighs 8.5
tons, and 5.5 tons
when it is empty.
2016, June 05 -- The project
manager Fernando Hisas (CONAE) said during
a conference that the VEX 5A
rocket will be launched in
July or August.
2015, Nov. 16 -- It is reported that a static test of the new
engine T10, used for the first stage of VEX 5A, was successful. The
engine has, as expected, no turbopump. The fuel supply carried out by means of compressed
gas.
2015, November -- new Tronador-II master plan
VEX 1A/1B: One stage with 4 tnf pressure fed engine (T4)
VEX 5A: One stage with new 10 tnf pressure
fed engine T10 (Kerosene/LOX)
VEX 5B: Two stage with new pressure fed
engine T10, and a other new pressure fed engine, using for the Tronador-II second
stage (Monomethyl-Hydrazine/N2O4+HNO3)
VEX 5C: Two stage with first stage 30
tnf engine T30 (Kerosene/LOX), using three times for the Tronador-II first
stage, and the pressure fed engine
2014, Aug. 16 -- Last night
VEX-1B was successfully launched.
Según informaron desde el Ministerio de Planificación Federal, el vehículo
lanzado concretó la trayectoria programada por espacio de 27 segundos y alcanzó
una altura máxima de 2200 metros.
2014, Feb. 26 -- El cohete despegó y explotó ?
El cohete de prueba del proyecto Tronador II, se lanzó esta mañana. Según
nos cuentan gente cercana al proyecto se habría elevado 2 metros y explotó. Sin
anuncios oficiales y con varios meses de demora, fue lanzado de manera fallida el
cohete VEX-1A que iba a ser utilizado para probar
sistemas de navegación.
En enero se había abortado el lanzamiento cuando falló una manguera de combustible,
desde entonces no se hicieron nuevos anuncios. Aunque siendo un cohete de prueba
estaba previsto que lo finalmente ocurrido pudiera pasar.
CONAE says the vehicle didn't explode. They say the engine started but the
"take off didn't happen".
Conrado Varotto, Executive Director of CONAE, said ealier in an interview, that
CONAE had conducted three tests of the engine on the ground, all three unsuccessful,
with a fourth test planned for mid-December (2013). The engine exploded in the first
two tests, due to liquid fuel leaks, and failed on the third, due to materials problems
with the exhaust. Varotto noted that CONAE has no intention of attempting a launch
until the engine is thoroughly and successfully tested on the ground.
|