Thursday, April 11, 2019

SpaceX - Falcon Heavy 2 - ARABSAT-6A

  SpaceX Falcon Heavy FH 2 - ARABSAT-6A - Launching April 11, 2019

Screenshot of Tim Dodd’s Youtube video about Falcon Heavy Arabsat-6A - Photo of FH-1

Mission Rundown: Falcon Heavy - ARABSAT-6A

Written: January 8, 2021

Lift Off Time

April 11, 2019 - 22:36 UTC - 18:36 EDT

Mission Name

ARABSAT-6A

Launch Provider

SpaceX

Customer

ArabSat

Rockets

Block 5 Sideboosters B1052-1 -Y

Falcon Heavy Block 5 Core booster B1055

Block 5 Sideboosters B1053-1 +Y

Launch Location

Launch Complex 39A - LC 39A at Kennedy Space Center

Payload

A2100 Bus Communication Satellite

Payload mass

6 000 kg ~ 13 228 pounds

Where is the satellite going?

ArabSat 6A is deployed in Geostationary Earth Orbit. The Supersynchronous Transfer Orbit has a perigee of 327 km, apogee at 89 815 km and 22,96° inclination.

Will they attempt to recover the first stage + side boosters?

Yes - The side boosters have enough fuel to return and the core booster is aiming for OCISLY

Where will the first stage and sideboosters land?

On OCISLY 967 km ~ 601 miles downrange and Landing Zones LZ-1 & LZ-2 back at CCAFS

Will they be attempting to recover the fairings?

Yes - Go Pursuit and Go Searcher will “Go Fish” 1029 km downrange due east of launch site

Are these fairings new?

Fairing types described in last chapter

Yes - Type 2.2 lifeboat sized fairings - 34 x 17 feet with 8 ventilation ports and a heat resisting steel tip

This will be the:

The Falcon Heavy core booster did make it to OCISLY 967 km downrange, but a lack of ability to secure the core booster by the Octagrabber resulted in the loss of the core booster when waves and the winds made it tumble over the railing.

The 38th landing became the 38th crash landing - Ironic to say the least

– 2nd Falcon Heavy launch by SpaceX

– 1st flight of Falcon Heavy Block 5 core booster

– 1st & 2nd flight of Falcon Heavy B5 side boosters

– 17th SpaceX launch from LC-39A

– 36tht, 37th & 38th booster landings overall

– 38th crash landing. soft, hard, deliberate, Ups…

– 2nd loss of a Falcon 9 core booster

– 4th mission for SpaceX in 2019

Where to watch

Where to read more

SpaceX Falcon Heavy FH-2

Tim Dodd on Falcon Heavy 2 April 11, 2019


Launch debriefing

(This is what happend)

-

-

T-00:15:17

T 00:00:00

T+00:01:12

T+00:02:36

T+00:02:53

T+00:03:37

T+00:03:43

T+00:04:10

T+00:06:14

T+00:07:05

T+00:07:29

T+00:08:55

T+00:09:32

T+00:26:40

T+00:27:38

-

T+00:33:27

T+00:34:06

T+00:34:33

-

Pre Launch Run Down at 3:20

Tim Dodd onsite but having technical difficulties

Sorry - Going to SpaceX live feed at: 4:39

Liftoff at 19:57

MaxQ at 21:09 (2-3 sec delay on downlink camera)

BECO at 22:31 Booster release at 22:33

Boost back burn by boosters at 22:50 - 76 seconds

MECO 23:32, stage separation 23:34

SES-1 at 23:40

Fairing separation at 24:07

Boosters entry burn 26:11 by 6 Merlin 1D# 13 seconds

Entry burn 27:03 by center core for 27 seconds ?

Landing burn 27:26 by 2 Merlin 1D# for 20 seconds

SECO-1 at 28:52 and coasting

Landing burn 29:29 by center core for 19 seconds ?

SpaceX resumes live feed at 46:37

SES-2 - SECO-2 in 87 seconds gave a velocity boost from 26 572 km/h to 36 701 km/h at 47:35

SpaceX resumes live feed at 53:24

Deploying ARABSAT-6A at 54:03

John Insprucker, Jessica Anderson and Alex Siegel raps up from SpaceX at 34:30



Sorry no ARABSAT-6A mission view available from Geoff Barrett. STP-2 still is though

What do you mean, Infidel? Fly a cheaper Falcon 9?

SpaceX will be launching its second Falcon Heavy rocket carrying the Arabsat-6A communications satellite to orbit. This Falcon Heavy is brand new, composed of two block 5 side boosters (B15052 & B1053) and a single reinforced block 5 core booster (B1055).

The launch window for this mission opens at 22:36 UTC on April 11, 2019 and is just about 2 hours in duration. The Falcon Heavy will be lifting off from Launch Complex 39A (LC-39A) at the Kennedy Space Center in Florida.

After burning for about 2 and a half minutes, the side boosters will separate from the core booster and boost back to the launch site for a landing at Landing Zones 1 & 2 (LZ-1 & LZ-2). The core booster will continue burning for another minute, before shutting down and separating from the second stage.

The core booster will be landing approximately 967 km (601 miles) downrange on the Autonomous Spaceport Drone Ship, Of Course I Still Love You (OCISLY).

Screenshot from SpaceX Webcast of ARABSAT 6A deployment

Unfortunately the core booster B1055 could not be secured to the Drone Ship by the Octa grabber, so it was lost at sea. The engine bay’s refitting as a center core and that made it hard to grab and hold down. Strong winds were blowing and the waves were too rough according to twitter, so the center core tumbled over the railing.

Likewise it wasn’t possible to transfer crew members aboard OCISLY safely so they could manually secure the core booster with heavy duty chains and support tripods. The weather was too rough and the risk of losing crew members washing overboard or getting hurt by loose equipment was too great.

Working on a chain gang. B1031-2 “I’ll be back” is back in Port Canaveral. Photo: John Krauss.

This picture of a ‘chain gang’ bringing a Falcon 9 booster home to port will tell you why. Its 4-5 meters up to those gray chain latches covering the ‘hold down’ clamps used during lift off to prevent Falcon 9 from taking off prematurely.

It takes two men to lift it and bolt it to that ‘hold down’ clamp, two chains had to be bolted on as well and attached/welded to the deck, while a hydraulic piston from a tripod lifts the entire Falcon 9 booster and stabilizes it vertically. Finally the chains are tightened so the booster is secure from lateral movement.

Now repeat this three more times in heavy seas and high winds. Good luck with that.

The Payload

Arabsat-6A is a geostationary communications satellite operated by Arabsat. The satellite was built by Lockheed Martin Space Systems on a modernized A2100 bus. Arabsat 6A is based on an updated version of the A2100 bus and is considered among the most advanced communications satellites built. The spacecraft utilizes fixed and steerable Ku-band and Ka-band transponders to provide TV and radio services to the Middle East and North Africa from its station at 30.5°East.

I’m getting the feeling that Arabsat-6A is flying Falcon Heavy for prestige reasons only.

Falcon Heavy Block 5

Falcon Heavy is a partially reusable heavy-lift launch vehicle designed and manufactured by SpaceX. It is derived from the Falcon 9 vehicle and consists of a strengthened Falcon 9 first stage as the center core with two additional Falcon 9-like first stages as strap-on boosters. Falcon Heavy has the highest payload capacity of any currently operational launch vehicle, and the third-highest capacity of any rocket ever to reach orbit, trailing the Saturn V and Energia.

The combined thrust of the Falcon Heavy 27 Merlin 1D# is 2/3 of the first stage thrust of the five F1 engines on the Saturn V rocket that lifted mankind through the atmosphere on its way to the Moon. This means that Falcon Heavy is almost capable of a Lunar mission like the Apollo Saturn V was. Two launches of Falcon Heavy should be able to do it.

Falcon Heavy consists of a structurally strengthened and therefore heavier Falcon 9 as the "core" component, with two additional Falcon 9 first stages without interstages but with nose cone acting as liquid fuel strap-on boosters, which is conceptually similar to Evolved Expendable Launch Vehicle (EELV) Delta IV Heavy launcher.

The rocket was designed to meet or exceed all current requirements of human rating. The structural safety margins are 40% above flight loads, higher than the 25% margins of other rockets. The Falcon 9 tank walls and domes are made from Aluminium–lithium alloy. SpaceX uses an all-friction stir welded tank. Falcon Heavy was designed from the outset to carry humans into space and it would restore the possibility of flying crewed missions to the Moon or Mars.

The interstage, which connects the upper and lower stage for Falcon 9, is a carbon fiber aluminum core composite structure. Stage separation occurs via reusable separation collets and a pneumatic pusher system. The second stage tank of Falcon 9 is simply a shorter version of the first stage tank and uses most of the same tooling, material, and manufacturing techniques. This approach reduces overall costs during production.

The Falcon Heavy includes first-stage recovery systems, to allow SpaceX to return the first stage boosters to the launch site as well as recover the first stage core following landing at an Autonomous Spaceport Drone Ship barge after completion of primary mission requirements. These systems include four deployable landing legs, which are locked against each first-stage tank core during ascent. Excess propellant reserved for Falcon Heavy first-stage recovery operations will be diverted for use on the primary mission objective, if required, ensuring sufficient performance margins for successful missions.

The nominal payload capacity to a geostationary transfer orbit (GTO) is 8,000 kg (18,000 lb) with recovery of all three first-stage cores versus 26,700 kg (58,900 lb) in fully expendable mode. The Falcon Heavy can also inject a 16,000 kg (35,000 lb) payload into GTO if only the two boosters are recovered.

In 2011, NASA Ames Research Center proposed a Mars mission called Red Dragon that would use a Falcon Heavy as the launch vehicle and trans-Martian injection vehicle, and a variant of the Dragon capsule to enter the Martian atmosphere.

The proposed science objectives were to detect biosignatures and to drill 1 m (3 ft 3 in) or so underground, in an effort to sample reservoirs of water ice known to exist under the surface. SpaceX 2015 estimation was 2,000–4,000 kg (4,400–8,800 lb) to the surface of Mars, with a soft retro propulsive landing following a limited atmospheric deceleration using a parachute and heat shield.

Beyond the Red Dragon concept, SpaceX was seeing potential for Falcon Heavy and Dragon 2 to carry science payloads across much of the Solar System, particularly to Jupiter's moon Europa. SpaceX announced in 2017 that propulsive landing for Dragon 2 would not be developed further, and that the capsule would not receive landing legs.

Consequently, the Red Dragon missions to Mars were canceled in favor of Starship, a larger vehicle using a different landing technology.

Just venting: Rare sights to behold

At 47:28 please pay attention to the large Oxygen ice crystal bouncing around during engine chill. It’s being blown loose by the increased Oxygen venting from LOX tank, like when a freezer venting a “hot” gas will remove heat from the LOX tank, and it’s used on its way out to chill the Turbopump. Fun fact of rocket mechanics.

And watch it being blasted by the Merlin 1D# vacuum engine at SES-2.

Another fun fact is that the flame trench below Falcon Heavy hasn't seen this kind of exhaust plumes since Space Shuttle and Saturn V. This can be seen on this screenshot where the very black smoke is evidence of the flame trench being blasted clean.

Who said the flame trench had been cleaned since April 2011? Don't you think he lied?

My fault for not remembering FH-1. It must have blasted that flame trench clean that day.

If it had rained recently then dirty rain water would have been in the flame trench, and the sod from all the previous 16 Falcon 9 launches and ignition test would have murked the rain water. If a drain pipe was clogged that too would have added to the exhaust smoke.

The Watertower must be working overtime to pump all that fire suppressant deluge water on the launchpad. The drop from the tower tank by itself could do it without pumps, but I don’t know for sure, if there isn't a pump or two available.

By the way, let's strap some booster to that Water Tower and see what happens.

Author Trevor Sesnic link

Coauthor/Text Retriever Johnny Nielsen

link to launch list


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