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Antares ready for inaugural flight

Posted by Jason Davis

11-04-2013 9:48 CDT

Topics: International Space Station, private spaceflight, rockets

There's nothing quite like the inaugural flight of a new rocket. Years and years of design work, fabrication, assembly, technical reviews, delays, artist concepts and press releases. All leading up to the moment of engine ignition and first motion, when the hard work of countless individuals comes to life and rises from the launch pad.

It's been a long, delay-ridden road for Dulles-based private spaceflight company Orbital Sciences Corporation. Their Antares rocket is finally ready for its April 17 inaugural flight. If all goes well, Antares will loft a payload meant to simulate their Cygnus spacecraft into the same, 51.6 degree orbit as the International Space Station. The demo payload will cruise around the Earth at just over half of the station's altitude in a 250 x 350 kilometer orbit (ISS is currently orbiting at 403 x 418 kilometers).

Antares ready for inaugural flight

NASA / Brea Reeves

Antares ready for inaugural flight
The full Antares rocket stack stands on the launch pad prior to its inaugural flight. The A-ONE mission will place a Cygnus payload simulator into orbit.

Orbital is NASA's second funded Commercial Orbital Transportation Services (COTS) partner. The other is SpaceX, which has now sent their Dragon capsule to the station three times. If this flight – officially termed A-ONE – goes well, Orbital says they could be ready mid-year to send a real Cygnus spacecraft to the ISS, which would complete their COTS demonstration requirements and pave the way for official paid cargo runs.

A basic Cygnus spacecraft has a pressurized volume of about 19 cubic meters. That's almost double what Dragon offers, but Cygnus lacks return cargo capability. It will act as a trash disposal unit for the ISS and burn up in the atmosphere. Cygnus berths to the station the same way Dragon does, by easing gently into the reach of Canadarm for berthing at the Unity module.  

Cygnus approaches the ISS

Orbital Sciences Corporation

Cygnus approaches the ISS
Orbital Sciences Corporation's Cygnus spacecraft approaches the International Space Station.

Cygnus's ride to orbit, Antares, is a two-stage launch vehicle. The first stage is fueled by liquid oxygen and kerosene, just like SpaceX's Falcon 9 rocket. It is powered by two Aerojet AJ-26 engines. These engines are Soviet-built, refurbished NK-33 engines that were originally built for the massive N1 launch vehicle that was designed to take cosmonauts to the moon. The second stage is solid-fueled, and powered by a single, ATK-built CASTOR 30 engine.

Originally, Antares was developed under the moniker Taurus II. Orbital shed the Taurus moniker in late 2011 and renamed the vehicle after the bright red star in the constellation Scorpius. The Taurus name received a lot of bad publicity after its last two missions ended in failure. NASA lost the Orbiting Carbon Observatory (OCO) in February 2009, and the Glory climate satellite in March 2011. Both accidents occurred after the Taurus's payload fairing failed to separate properly. NASA was originally willing to give Taurus a third try for OCO-2, but ended up switching to the recently-resurrected Delta II.

Antares A-ONE vehicle configuration

Orbital Sciences Corporation

Antares A-ONE vehicle configuration
A breakdown of the Antares launch vehicle, as configured for the A-ONE demonstration flight.

Antares and the Cygnus simulation payload are scheduled to launch Wednesday, April 17 at 5 p.m. EDT (21:00 UTC). The launch window lasts for three hours, and there are backup opportunities the following four days. The launch will take place from pad 0A at the Mid-Atlantic Regional Spaceport (MARS), home of the NASA Wallops Flight Facility. 

MARS has two operational launch pads: 0A for "mid-class" launch vehicles, and 0B for "small-class." Pad 0A accommodates a gross liftoff weight, or GLOW, of more than one million pounds, and is licensed for low-Earth orbit (LEO) payloads of up to 11,000 pounds. Pad 0B accommodates a GLOW of 750,000 pounds, and LEO payloads of up to 8,400 pounds.

Here is a timeline of launch events for the A-ONE flight, according to Orbital:

Event  Altitude (kilometers)  Elapsed time (mm:ss)
Stage 1 Ignition  0  00:00
Liftoff  0  00:02
Main Engine Cutoff (MECO)  107  03:50
Stage 1 Separation  113  03:55
Fairing Separation  184  05:19
Stage 2 Ignition  189  05:28
Stage 2 Burnout  256  08:03
Payload Separation  255  10:03
 
See other posts from April 2013

 

Or read more blog entries about: International Space Station, private spaceflight, rockets

Comments:

Bob Ware: 04/11/2013 10:59 CDT

Hi Jason. This is a very informative article. Thanks. One question. S2 Burnout to payload Sep has a drop of 1 km. Is that an entry error or is the vehicle intended to fall back prior to Sep? Thanks.

Jason Davis: 04/11/2013 03:03 CDT

Hi Bob, it's not a typo -- at stage 2 burnout, the vehicle is in orbit and its altitude will vary between 250 (perigee) and 350 (apogee) kilometers (according to Orbital's figures). So it will be very close to perigee when it separates, and then its altitude should start increasing after that. At least, as I understand it.

Andy Hastings: 04/11/2013 06:06 CDT

I am confused. Is there a minute and a half of coasting between MECO/stage 1 separation and stage 2 ignition?

Bob Ware: 04/12/2013 12:15 CDT

Jason - Duh... and thanks! LOL!!! How did I miss that?! LOL!! I know better : (

Jason Davis: 04/14/2013 04:25 CDT

Andy - Yep, exactly right. Check out this thread for some chatter about why that is: http://forum.nasaspaceflight.com/index.php?topic=15457.215;wap2

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