Launch News AEHF-2 atop Atlas V-531 (AV-031) on May 4, 2012

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The United Launch Alliance Atlas 5 rocket (AV-031) will launch the second Advanced Extremely High Frequency (AEHF) satellite. Built by Lockheed Martin, this U.S. military spacecraft will provide highly-secure communications. The rocket will fly in the 531 vehicle configuration with a five-meter fairing, three solid rocket boosters and a single-engine Centaur upper stage.

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Launch date:​
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May 4, 2012​
Window open:​
18:42 UTC / 2:42 p.m. EDT
Window close:​
20:42 UTC / 4:42 p.m. EDT
Launch site:​
| SLC-41, CCAFS, Florida

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[highlight]L[eventtimer]2012-5-4 18:42;%c%%ddd%/%hh%:%mm%:%ss%[/eventtimer][/highlight]​
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Scrubbed on May 3 due to purge problem for the Centaur interstage adapter.


There is calendar event created for this launch, for which you can request a reminder.


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Mission Insignia (clickable)​

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Viewing the Launch Live:
A live simulcast of the launch broadcast will begin 20 minutes before opening of the launch window, at 18:22 UTC / 2:22 p.m. EDT:
Alternate video streams:



Payload:
The AEHF (Advanced Extreme High Frequency Satellite), a.k.a. AWS (Advanced Wideband Satellite), program is the next generation of highly secure, high capacity, survivable communications to the U.S. warfighters during all levels of conflict, and will become the protected backbone of the Department of Defense's military satellite communications architecture. The AEHF system will be integrated into the legacy Milstar (Military Strategic & Tactical Relay) constellation, and will be backward compatible with Milstar's low data rate (LDR) and medium data rate (MDR) capabilities, while providing extreme data rates (XDR) and larger capacity at substantially less cost than the Milstar system. Each satellite will be launched on an Evolved Expendable Launch Vehicle (EELV), with the first launch planned for April 2008. They cost approximately $580 million per satellite

On-board signal processing will provide protection and ensure optimum resource utilization and system flexibility among the Armed Forces and other users who operate terminals on land, sea and air. The AEHF system will be integrated into the legacy Milstar constellation, and will be backward compatible with Milstar's low data rate (LDR) and medium data rate (MDR) capabilities, while providing extreme data rates (XDR) and larger capacity at substantially less cost than the Milstar system.

AEHF satellites feature following antennas:
  • 2 SHF Downlink Phased Arrays,
  • 2 Crosslinks,
  • 2 Uplink/Downlink Nulling Antennas,
  • 1 Uplink EHF Phased Array,
  • 6 Uplink/Downlink gimbaled Dish Antenna,
  • 1 Each Uplink/downlink earth coverage horns

Up to six satellites were planned, but in late 2004 it was decided, to end the AEHF program after the third satellite in favour of introducing the next generation T-Sat earlier. Problems with the T-Sat program might lead to procurement of two more AEHFs instead.

aehf-1__1.jpg


Type / Application:​
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  • Comsat
Operator:​
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  • USAF
Contractors:​
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  • Lockheed Martin (Bus),
  • Northrop Grumman (ex TRW) (Payload)
Configuration:​
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  • A2100M
Propulsion:​
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  • IHI BT-4,
  • HCT
Power:​
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  • 2 deployable 5 segment solar arrays,
  • batteries
Lifetime:​
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  • 14 years
Mass:​
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  • 6168 kg
Orbit:​
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  • GEO



Launch Vehicle:

Atlas-5.jpg
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The Atlas 5 was developed by Lockheed Martin Commercial Launch Services as part of the US Air Force Evolved Expendable Launch Vehicle (EELV) program. Each Atlas 5 rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage.​
The rocket will fly in the 531 vehicle configuration with a five-meter fairing, three solid rocket boosters and a single-engine Centaur upper stage.​
Rocket stages / engines:[table="head;width=500"]Strap-On|Stage 1|Stage 2

3 × SRB|CCB / RD-180|Centaur-5-SEC / RL-10A4-2​
Performance:[table="head;width=500"]LEO|LPEO|SSO|GTO|GEO|MolO|IP

15300 kg|12185 kg|11160 kg|7425 kg|3250 kg||[/table]​
[/table]​



Launch Preparations:
Encapsulation:
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Click on images to enlarge

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Mating:
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Click on images to enlarge

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Rollout:
[table="head"]{colsp=4}
Click on images to enlarge

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On the pad:
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Click on images to enlarge

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Countdown Timeline:
[table="head;width=500"]
T [HH:MM]
|
UTC
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EDT
|Event

-6:20 ​
|
11:42 ​
|
7:42 a.m. ​
|Countdown begins with rocket power up

-5:30 ​
|
12:32 ​
|
8:32 a.m. ​
|Weather briefing

-4:55 ​
|
13:07 ​
|
9:07 a.m. ​
|Start clearing assembly building area

-4:20 ​
|
13:42 ​
|
9:42 a.m. ​
|C-band tracking beacon testing

-3:40 ​
|
14:22 ​
|
10:22 a.m. ​
|S-band telemetry link checks

-2:55 ​
|
15:07 ​
|
11:07 a.m. ​
|Establish blast danger area roadblocks

-2:20 ​
|
15:42 ​
|
11:42 a.m. ​
|Weather briefing

-2:15 ​
|
15:47 ​
|
11:47 a.m. ​
|Clear the pad

-2:00 ​
|
16:02 ​
|
12:02 p.m. ​
|T-120 minutes and holding (for 30min)

-2:00 ​
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16:27 ​
|
12:27 p.m. ​
|Launch conductor briefing to team

-2:00 ​
|
16:29 ​
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12:29 p.m. ​
|Readiness poll for fueling

-2:00 ​
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16:32 ​
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12:32 p.m. ​
|Resume countdown

-1:50 ​
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16:42 ​
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12:42 p.m. ​
|Centaur LOX transfer line chilldown

-1:43 ​
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16:49 ​
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12:49 p.m. ​
|Begin Centaur liquid oxygen loading

-1:30 ​
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17:02 ​
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1:02 p.m. ​
|Begin Atlas first stage LOX loading

-1:25 ​
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17:07 ​
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1:07 p.m. ​
|Centaur LH2 transfer line chilldown

-1:10 ​
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17:22 ​
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1:22 p.m. ​
|Centaur RL10 engine chilldown

-1:02 ​
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17:30 ​
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1:30 p.m. ​
|Begin Centaur liquid hydrogen loading

-0:40 ​
|
17:52 ​
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1:52 p.m. ​
|FLight termination system final test

-0:16 ​
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18:16 ​
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2:16 p.m. ​
|RD-180 engine fuel fill sequence

-0:10 ​
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18:22 ​
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2:22 p.m. ​
|Weather briefing

-0:04 ​
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18:28 ​
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2:28 p.m. ​
|T-4 minutes and holding (for 10min)

-0:04 ​
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18:35 ​
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2:35 p.m. ​
|Readiness poll for launch

-0:04 ​
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18:38 ​
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2:38 p.m. ​
|Resume countdown

-0:00 ​
|
18:46 ​
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2:42 p.m. ​
|LAUNCH[/table]​



Launch Timeline & Ground Track:
[table="head;width=500"]
T [MM:SS]
|
Event

-00:02.7​
Engine Start

{colsp=2}
The Russian-designed RD-180 main engine is ignited and undergoes checkout prior to launch.


+00:01.1​
Liftoff

{colsp=2}
The three strap-on solid rocket boosters are lit as the Atlas 5 vehicle, designated AV-031, lifts off and begins a vertical rise away from Complex 41 at Cape Canaveral Air Force Station, Florida.


+01:56.0​
Jettison SRBs

{colsp=2}
Having burned out of propellant approximately 25 seconds earlier, the spent solid rocket boosters are jettisoned to fall into the Atlantic Ocean.


+03:34.0​
Nose Cone Jettison

{colsp=2}
The payload fairing that protected the AEHF 2 spacecraft during launch is separated once heating levels drop to predetermined limits.


+03:39.0​
Forward Load Reactor Jettison

{colsp=2}
The Forward Load Reactor deck that supported the payload fairing's structure to Centaur upper stage is released seconds after the shroud's jettison.


+04:18.0​
Main Engine Cutoff

{colsp=2}
The RD-180 main engine completes its firing after consuming its kerosene and liquid oxygen fuel supply in the Atlas first stage.


+04:24.0​
Stage Separation

{colsp=2}
The Common Core Booster first stage of the Atlas 5 rocket separates from the Centaur upper stage. Over the next few seconds, the Centaur engine liquid hydrogen and liquid oxygen systems are readied for ignition.


+04:34.0​
Centaur Ignition 1

{colsp=2}
The Centaur RL10 engine ignites for the longer of the two upper stage firings. This burn will inject the Centaur stage and AEHF 2 spacecraft into a parking orbit.


+13:57.0​
Centaur Cutoff 1

{colsp=2}
The Centaur engine shuts down after arriving in a planned parking orbit. The vehicle enters a brief coast period lasting nearly 8 minutes before arriving at the required location in space for the second burn.


+22:06.0​
Centaur Ignition 2

{colsp=2}
The Centaur re-ignites over the equatorial Atlantic to accelerate the payload into geosynchronous transfer orbit from the parking achieved earlier in the launch sequence.


+27:48.0​
Centaur Cutoff 2

{colsp=2}
At the conclusion of its second firing, the Centaur will have delivered the AEHF 2 spacecraft into the targeted orbit with an apogee of 31,070 statute miles, perigee of 140 statute miles and inclination of 21 degrees.


+51:11.0​
Spacecraft Separation

{colsp=2}
The U.S. military's second Advanced Extremely High Frequency communications satellite is released into orbit from the Centaur upper stage to complete the AV-031 launch.
[/table]

map_full.jpg



Links:
 
geeez,

How many comm. satellites does the military need?
 
A lot. By summing the mass of all those during the few last years, there is probably enough to build another ISS :lol:
 
geeez,

How many comm. satellites does the military need?

Too many?
Seriously, it's a pity that the EELV's are just flying because of military- and NROL-toys, maybe a probe every few years.
 
But that was the purpose of EELV program, to reduce cost for military. Unfortunately, "reduced cost" rockets are still far too expensive for the commercial market.

They do launch GPS and the occasional weather sat., though. :hmm:
 
Now 30 minutes from liftoff.


NASASpaceflight: ULA Atlas V set to launch AEHF-2 communications satellite


Spaceflight Now: Mission Status Center:

1814 GMT (2:14 p.m. EDT)
The launch team is looking at a possible ground problem with the purge flow to the vehicle. Engineers are assessing.

{...}


1748 GMT (1:48 p.m. EDT)
The weather odds have increased to 90 percent favorable for an on-time launch of the Atlas 5 rocket today.

Still calling for scattered clouds at 3,000 feet, scattered high clouds at 25,000 feet, a chance of isolated coastal showers, good visibility, southeasterly winds of 16 to 20 knots and a temperature around 79 degrees F.

 
Live coverage started.


Delay-
They need to re-enter pad to manually flip a "misconfigured" valve.
 
Last edited:
Not coming out from the hold until resolution of the issue. No new T-0 yet set.
 
SCRUB. 24-hour recycle.

Tomorrow's window opens at 18:42 UTC / 2:42 p.m. EDT.


SPACE.com: US Air Force Satellite Launch Delayed by Glitch

Florida Today: Atlas Launch Scrubbed, Reset For Friday


Weather update:
The weather forecast for Friday calls for another day of 80 percent favorable odds of launching the Atlas 5 rocket. Clouds will be the only slight concern.

The outlook calls for scattered clouds at 3,000 feet, scattered high clouds at 25,000 feet, a chance isolated showers, good visibility, southeasterly winds of 12 to 16 knots and a temperature around 79 degrees F.
 
The United Launch Alliance Atlas Launch

I see they just scrubbed the launch for today due to a manual valve problem and a stray frequency downrange, southeast of the pad. Anyone know what this frequency might be from? A ship? Does this happen often? Just wondering.

Andrew
 
Spaceflight Now: Mission Status Center:
1400 GMT (10:00 a.m. EDT)The purge system for the Centaur interstage adapter has been successfully retested following corrective work by technicians to reconfigure a manually-operated control valve on the mobile launch platform. Engineers recently completed a helium flow test to validate the entire system and the results looked nominal, officials say, clearing the way for today's launch at 2:42 p.m. EDT.

1310 GMT (9:10 a.m. EDT)It is shaping up to be a cloudier day for this second launch attempt, forecasters report. Meteorologists will be watching for electrically charged anvil clouds from thunderstorms in the Gulf of Mexico coming over the launch site and the thickness of the local cloud cover as potential violations to the launch rules this afternoon. Overall, there is a 70 percent chance of acceptable weather.

The outlook calls for scattered clouds at 3,000 and 10,000 feet, broken high clouds at 24,000 feet, a chance isolated coastal showers, good visibility, southeasterly winds of 12 to 16 knots and a temperature around 79 degrees F.

Forecasters predict similar conditions and 70 percent odds on Saturday, if the launch is delayed again for some reason.

Florida Today: Atlas V will try to fly again today
 
Now at L-30 minutes. The live coverage should begin in 10 minutes.
 
The live coverage is starting now.
 
T-4 minutes and counting.

Here's a look at some stats about today's mission. This will be:
  • The 612th launch for Atlas program since 1957
  • The 324th Atlas to occur from Cape Canaveral
  • The 201st mission for Centaur upper stage
  • The 178th use of Centaur by an Atlas rocket
  • The 30th launch of an Atlas 5 since 2002
  • The 26th Atlas 5 to occur from the Cape
  • The 22nd Atlas 5 under United Launch Alliance
  • The 49th Evolved Expendable Launch Vehicle flight
  • The 9th Atlas 5 launch overseen by the Air Force
  • The 10th 500-series flight of the Atlas 5
  • The 2nd Atlas 5 to fly in the 531 configuration
  • The 2nd Atlas launch with AEHF payload
  • The 2nd Atlas launch of 2012
 
Liftoff has occurred at the beginning of the launch window.
 
The powered stages of the flight has ended. S/C separation is scheduled in 20 minutes.
 
I wouldn't consider that disco...
 
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