Launch data:
| Designation | A08335 / 15U01 |
| Launch date | 11 Feb 2015 - 13:40 UT |
| Launch site | Kourou, ZLV |
| Launch vehicle |
Vega (VV04) |
| Mission | Technology |
| Suborbital Flight: |
| Perigee / Apogee | 220 x 430 km |
| Eccentricity | |
| Inclination | 5.4° |
| Period | min |
Launched together with: IXV
Spacecraft data:
| Prime manufacturer | Thales Alenia Space Italy |
| Platform | |
| Operator | |
| Mass at launch | |
| Empty Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
|
End of live:
| Re-entered date: | 11 Feb 2015 - around 16:00 UT |
| Lifetime: | |
|
Launched into a suborbital trajectory on ESA’s small Vega rocket from Europe’s Spaceport in French Guiana, the vehicle will return
to Earth as though from a low-orbit mission. For the first time, it will test and qualify European critical reentry technologies in
hypersonic flight, descend by parachute and land in the Pacific Ocean to await recovery and analysis.
Description:
- A European Vega rocket, designated VV04, will launch with the European Space Agency’s Intermediate Experimental Vehicle, or
IXV. The IXV will launch on a suborbital trajectory, testing advanced flight control and re-entry technologies before splashing down
in the Pacific Ocean.
- The Intermediate eXperimental Vehicle (IXV) is an European Space Agency (ESA) experimental re-entry vehicle intended to validate
European reusable launchers that could be evaluated in the frame of the Future Launchers Preparatory Programme (FLPP). The IXV development
would be carried out under the leadership of the NGL Prime SpA company. It would inherit the principles of previous studies such as
CNES's Pre-X and ESA's AREV (Atmospheric Reentry Experimental Vehicle).
- IXV uses a lifting body arrangement with no wings of any sort, using two movable flaps for re-entry flight control. Re-entry is
accomplished in a nose-high attitude like the Space Shuttle, with manoeuvring accomplished by rolling out-of-plane and then lifting in
that direction, like an aircraft. Landing is accomplished by parachutes ejected through the top of the vehicle. The airframe is based
on a traditional hot-structure/cold-structure arrangement, and is supported on-orbit by a separate manoeuvring and support module
similar to the Resource Module intended for the Hermes. The avionics are controlled by a LEON2-FT microprocessor, and interconnected
by a MIL-STD-1553B serial bus.
Pre-launch testing:
- The IXV's subsonic parachute system was tested at the Yuma Proving Ground in Arizona in late 2012. Water impact tests were
conducted at Consiglio Nazionale delle Ricerche's INSEAN research tank near Rome.
- On 21 June 2013 an IXV test vehicle was dropped from an altitude of 3 kilometres (1.9 mi) in the Salto di Quirra range off Sardinia.
The test was to validate the water landing system including the subsonic parachute, floatation balloons, and beacon deployment. A small
anomaly was encountered when inflating the balloons, but the other systems performed as expected. After the test the vehicle was taken
for further analysis.
- On 23 June 2014 the recovery ship Nos Aries conducted a training exercise with an IXV test article off the coast of Tuscany.
- In June 2014 the IXV test vehicle arrived at the ESTEC Technical Centre in Noordwijk, the Netherlands, to undergo a rigorous test
campaign to confirm its flight readiness in anticipation of a flight on a Vega rocket in November.
Mission details:
- Delayed from October and Nov. 18, 2014.
- The Arianespace/ESA Vega rocket made its fourth flight from Kourou on Feb 11.
The Vega VV04 took off at 1340 UTC, with the AVUM 4th stage entering a 76 x 416 km x 5.4 deg orbit at 1353 UTC.
- The AVUM stage made a second burn at apogee at 1411 UTC. Although details have not been officially revealed, according to the
Novosti Kosmonavtiki forum, it entered a 220 x 430 km x 5 deg orbit. A third burn followed at 1529 UTC as the AVUM passed over Kourou
again, to deorbit the stage after one trip around Earth; the AVUM reentered over the Indian Ocean around 1600 to 1615 UTC.
- By traditional NORAD rules, the AVUM stage should have received a launch number of 2015-007 and a catalog number, but this appears not to have happened.
External links:
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Ref.: #7(JR708-709) - update: 05.05.15 |
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