Author Topic: Proton-M/DM-03 - Elektro-L № 3 - Baikonur 81/24 - Dec 24, 2019 (12:03 UTC) (Read 32309 times)

zandr · « **Reply #20 on:** 02/25/2019 04:14 am »

https://ria.ru/20190225/1551318376.html
Google translate:

Quote

MOSCOW, February 25 - RIA News. The launch of the Electro-L meteorological satellite number 3 will take place at the end of November 2019, a source in the rocket and space industry told RIA Novosti on Monday.
Earlier, the Lavochkin NPO, which manufactures the third satellite Electro-L, reported that its launch is scheduled for October 2019.
"The sending of the Electro-L satellite number 3 into space by the Proton-M rocket with the upper stage DM-03 from the Baikonur cosmodrome is scheduled for November 20, 2019," a spokesman said...

Stan Black · « **Reply #21 on:** 06/12/2019 04:07 pm »

Proton-M №93566

zubenelgenubi · « **Reply #22 on:** 07/17/2019 01:48 pm »

Cross-post:

Quote from: Salo on 07/17/2019 08:30 am

https://ria.ru/20190717/1556597987.html
Google translate:
Quote
MOSCOW, July 17 - RIA News. The next meteorological satellite, Electro-L, is scheduled to be launched by the Proton-M launch vehicle with a DM-03 upper stage from the Baikonur launch site in December 2019, according to the "Sineva" edition, produced by the Krasnoyarsk Machine-Building Plant.
...
The Krasnoyarsk Machine-Building Plant manufactured and sent to the Rocket and Space Corporation Energia a basic module 11С861-03 (upper stage DM-03 - ed.) №6L for the Proton-M launch vehicle. In December 2019, using it the orbit will be launched one of the meteorological satellites, "- says in the magazine.

Re: use of launch pad 200/39

Quote from: anik on 06/14/2019 01:05 pm

It depends on what DM-03 upper stage will be used: if 3L then 81/24, if 6L then 200/39.

EDIT/ADD:

Quote from: anik on 07/17/2019 04:21 pm

Quote from: anik on 06/14/2019 01:05 pm
It depends on what DM-03 upper stage will be used: if 3L then 81/24, if 6L then 200/39

I have a correction: if 3L then 81/24, if 6L then 200/39 or 81/24.

zubenelgenubi · « **Reply #23 on:** 09/30/2019 08:34 pm »

Cross-post, including attachment:

Quote from: Salo on 09/30/2019 07:23 pm

http://raaks.ru/wp-content/uploads/2019/09/ОБЗОР-СТРАХОВАНИЯ-КОСМИЧЕСКИХ-РИСКОВ-2019.pdf

Launch date, as of this document's publication, is December 24, 2019.

zubenelgenubi · « **Reply #24 on:** 10/14/2019 12:09 am »

This is now the next Proton launch.
Has any hardware been delivered to Baikonur?

anik · « **Reply #25 on:** 10/14/2019 06:17 am »

Quote from: zubenelgenubi on 10/14/2019 12:09 am

Has any hardware been delivered to Baikonur?

No.

jacqmans · « **Reply #26 on:** 11/01/2019 08:03 am »

11/01/2019 10:00

A train with a Proton-M missile has been sent to Baikonur
On the night of November 1, 2019 at the GKNPTs im. M.V. Khrunicheva sent a train with blocks of the Proton-M launch vehicle, an upper stage and a head fairing to the Baikonur Cosmodrome.

All activities related to the sending of withdrawal funds were completed on a regular basis. The Proton-M launch vehicle with the DM-03 booster block created at RSC Energia (part of Roscosmos State Corporation) and the head fairing of the production of NPO Lavochkin (part of Roscosmos State Corporation) used to launch the Russian meteorological satellite "Electro-L" No. 3.

In addition, a full-size refueling model of the Briz-M booster block is transported as part of the railway echelon. Using a prototype, the cosmodrome specialists will conduct complex tests of the new refueling position of the Briz-M upper stage in the interests of the GKNPTs im. M.V. Khrunicheva.

https://www.roscosmos.ru/27706/

eeergo · « **Reply #27 on:** 11/13/2019 12:28 am »

https://twitter.com/roscosmos/status/1194163191938453504

zubenelgenubi · « **Reply #28 on:** 11/14/2019 01:22 am »

Cross-post:

Quote from: anik on 11/13/2019 06:38 pm

Quote from: Alter Sachse on 11/12/2019 07:48 pm
DM-03/3L or 6L

3Л, due to problems with 6Л.

GWR64 · « **Reply #29 on:** 11/30/2019 07:24 am »

https://twitter.com/roscosmos/status/1200019003042942976

tehwkd · « **Reply #30 on:** 12/10/2019 04:23 am »

24 1200-1240 UTC
25 1200-1240 UTC
26 1155-1235 UTC
27 1150-1230 UTC
28 1145-1225 UTC

Quote

J0022/19 - RESTRICTED AREA ACT: UNR1238. GND - UNL, 24 25 1200-1240, 26 1155-1235, 27 1150-1230, 28 1145-1225, 24 DEC 12:00 2019 UNTIL 28 DEC 12:25 2019. CREATED: 10 DEC 01:37 2019

zubenelgenubi · « **Reply #31 on:** 12/13/2019 02:56 am »

Quote from: tehwkd on 12/10/2019 04:23 am

24 1200-1240 UTC
25 1200-1240 UTC
26 1155-1235 UTC
27 1150-1230 UTC
28 1145-1225 UTC

Interesting how the NOTAM windows are the same for December 25 and 26, then come five mintues earlier per day on the 26th, 27th, and 28th. The launch time is apparently moving slowly earlier day by day.

Nicolas PILLET · « **Reply #32 on:** 12/16/2019 07:28 pm »

Elektro-L n°3 has number 1522.

tehwkd · « **Reply #33 on:** 12/20/2019 03:34 am »

launchpad notam posted.

24 1155-1215
25 1150-1210
26 1145-1205
27 1140-1200
28 1135-1155

Quote

K5264/19 - PROHIBITED AREA ACTIVATED WI 17NM RADIUS CENTRED ON 460224N 0630155E. SFC - UNL, 24 1155-1215, 25 1150-1210, 26 1145-1205, 27 1140-1200, 28 1135-1155, 24 DEC 11:55 2019 UNTIL 28 DEC 11:55 2019. CREATED: 20 DEC 02:25 2019

anik · « **Reply #34 on:** 12/20/2019 05:32 am »

12:03:02 UTC.

Magic · « **Reply #35 on:** 12/20/2019 07:44 pm »

At orbital position 165.8 E longitude will give a wx view across the Pacific Region, with a ~4° elevation from the NA west coast.

Galactic Penguin SST · « **Reply #36 on:** 12/21/2019 05:11 am »

The Proton has rolled out to the pad at Area 81 today:

https://twitter.com/roscosmos/status/1208258109615038466

anik · « **Reply #37 on:** 12/21/2019 09:18 am »

Quote from: Stan Black on 06/12/2019 04:07 pm

Proton-M №93566

Or 4921564069.

Also fairing 465ГК.Г-04 №322-01 (former АМГЭ, I think).

Galactic Penguin SST · « **Reply #38 on:** 12/21/2019 10:07 am »

There's quite a bit of snow falling at Baikonur as the Proton goes up on the launch pad!

https://twitter.com/roscosmos/status/1208323541021724672

GWR64 · « **Reply #39 on:** 12/21/2019 12:25 pm »

Are the limits for orbit margin known?
GEO is clear, but exact, like the Express-AM8 launch on Proton-M/DM03, or only quasi-GEO like Elektro-L2 on Zenit?
Can the Block-DM prove its precision?