TRACE

 1998-020A

---

The Transitional Region and Coronal Explorer was the 4th SMEX mission, to study magnetic fields and heating in solar corona. It returns the highest resolution EUV images of the sun. Mass is 250 kg; the bus was a GSFC SMEX. TRACE carries a 0.3m aperture Ritchey-Chretien telescope, with coatings for both optical-UV and EUV (narrow 171A, 195A and 284A bands) imaging. One quadrant of the primary observes in the UV, the remainder in the EUV. The telescope has an 8.5min field of view, and is derived from the NIXT sounding rocket and the EIT telescope on SOHO.

TRACE
Date	Time	Event	Orbit
1998 Apr 2	0144	L-1011 t/o from VAFB
	0242:39	Pegasus drop
	0242:44	Stage 1 burn
	0243:59	Stage 2 burn
	0245:06	Stage 2 MECO
	0249:55	Stage 2 sep
	0250:04	Stage 3 burn
	0251:12	Stage 3 MECO
	0252:12	Stage 3 sep
1998 Apr 2	1430		97.10 598 x 641 x 97.8
1998 Apr 20		First light
2017 Jun 21		end of science ops

Payload:

• TRACE telescope

• CCD camera

Space mission transcripts

 Freedom 7:

https://ia800607.us.archive.org/28/items/NasaAudioHighlightReels/MR03_TEC.PDF

Liberty Bell 7:

https://ia800607.us.archive.org/28/items/NasaAudioHighlightReels/MR04_TEC.PDF

Friendship 7:

https://ia600607.us.archive.org/28/items/NasaAudioHighlightReels/MA06_TEC.PDF

Aurora 7:

https://ia600607.us.archive.org/28/items/NasaAudioHighlightReels/MA07_TEC.PDF

Sigma 7:

https://ia800607.us.archive.org/28/items/NasaAudioHighlightReels/MA08_TEC.PDF

Faith 7:

https://ia800607.us.archive.org/28/items/NasaAudioHighlightReels/MA09_TEC.PDF

Gemini 3:

https://ia800607.us.archive.org/28/items/NasaAudioHighlightReels/GT03_PAO.PDF

https://ia600607.us.archive.org/28/items/NasaAudioHighlightReels/GT03_TEC.PDF

Shenzhou 10

 2013-029A

---

DV to docking 55 m/s for major burns, about 145 kg so mass about 7936 kg. Plus prox ops, say around 7900 kg at docking.

SZ10
Date	Time	Event	Orbit
2013 Jun 11	0938:03	Launch by CZ-2F	JQ
		T+2:00 LES sep
		T+2:34 SOB burnout, sep
		T+2:35 St 1 MECO
		T+2:36 St 1 sep, St 2 burn
		T+3:28 Fairing sep, 2 halves
		T+7:36 St 2 MECO
	0947	T+9:31 VECO
	0947	St 2 sep T+9:34	89.65 198 x 316 x 42.8
	1632?	DV1 19m/s	90.26 260 x 314 x 42.8
2013 Jun 12	1345?	DV2 28m/s	90.95 315 x 327 x 42.8
2013 Jun 13	0248	Begin V-bar approach
2013 Jun 13	0320?	DV3 7.5m/s	91.21 329 x 339 x 42.8
	0511	Docked
	0518	Hard dock
	0811?	Crew entry
2013 Jun 23
	0026	Undocked
		Stationkeep
		Begin V-bar approach
	0200	Docked
	0207	Hard docked
	0509	HO to TG-1
2013 Jun 24
	2107	HC to TG-1
	2305	Undocked
		Flyaround
2013 Jun 25	0025	Rerendezvous on V-bar
		Sep burn
	2321?	OM sep
	2323?	Deorbit
	2325?	DO CO
	2343	SM sep
	2354	Entry
2013 Jun 26
	0007	Landed 111.36E 42.33N

Soyuz TMA-07M (Sail)

 2012-074A

---

Soyuz TMA-07M (factory no. 704A, ISS flight 33S) was launched on 2012 Dec 19 with Roman Romanenko, Chris Hadfield and Tom Marshburn. 

Mass 1395 kg BO, 2893 kg SA, 880 kg prop, 7186 kg total. Spacecraft 704A used the SA from 708 and the BO and PAO from 707, following ground test damage to SA 704.

 

TMA07M
Date	Time	Event	Orbit
2012 Dec 19	1212:36	Launch by Soyuz-FG	Baikonur LC31
		T+1:53 SAS sep
		T+1:58 Blok-BVGD sep, 45 km
		T+2:37 GO sep
		T+4:47 Blok A sep
		T+4:57 KhO sep
	1221:21	T+8:45 Blok-I MECO
	1221:24	T+8:48 Blok-I sep
	1547:47	DV1 80.6s 32.65m/s
	1646:10	DV2 43.8s 17.71m/s
2012 Dec 20	1328:59	DPO burn 19s 1.3m/s
2012 Dec 21
	1213s	DV
	1235s	DV
	1259s	DV
	1340s	Braking
	1352	Begin flyaround at 300m
	1357	Stationkeeping
	1358	Final approach
	1402	Inside 75m
	1408:44	Docked with Rassvet
	1637	HO
2013 May 13
	1950	HC to ISS
	2307:54	Undocking from Rassvet after 143d 9h
	2310:54	15s sep burn
2013 May 14			410 x 416 km
	0137:09	SKD Deorbit 4:45 128.1m/s	-19 x 410
	0141:56	DO CO
	0204:55	Module sep
	0207:54	Entry interface 100 km
	0230:37s	Landing

Discovering the Cosmos with Small Spacecraft : The American Explorer Program

 https://welib.org/md5/5957c32a5fa62506839d80db733aa35d

The social climber's handbook : a shameless guide

https://welib.org/md5/6539c8f62a4b6c59518e8e10cd43f6da

Moonlight Beach

 https://www.dewolfemusic.com/search.php?id=28509150&code=6GZRjv

December 8,2019

 https://planet4589.org/space/jsr/back/news.772.txt

The Space Shuttle Program: Technologies and Accomplishments

 https://welib.org/md5/f12131f16e05a45498bc483d80ff29a8

Echostar 16

 2012-065A

---

SS/L Loral 1300 satellite for Echostar at 61.5W. Mass 6650 kg full 3520 kg dry.

Echo16
Date	Time	Event	Orbit
2012 Nov 20	1831:00	Launch by Proton-M	LC200/39
		T+1:55 MD2
		T+2:00 St 1 sep
		T+5:24 MD3
		T+5:27 St 2 Sep
		T+5:44 GO sep
	1840	T+9:42 St 3 MECO
		T+9:42 OB sep	-866 x 182 x 51.5
	1842	T+11:16 MES-1
	1849	T+18:42 MECO-1	176 x 177 x 51.5
	1938	T+1:07:43 MES-2
	1956	T+1:25:13 MECO-2	267 x 4996 x 50.3
	2159	T+3:28:06 MES-3
	2208	T+3:37:43 MECO-3
	2209	T+3:38:33 DTB sep	320 x 12396 x 49.7
	2211	T+3:40:01 MES-4
	2218	T+3:47:33 MECO-4	428 x 35814 x 49.1 (s)
2012 Nov 21	0325	T+8:54:20 MES-5
		T+8:58:55 MECO-5	2434 x 35786 x 29.5 (s)
	0343	T+9:11:46 Briz-M sep

November 25,2004

 https://en.wikipedia.org/wiki/English_poetry

Outpost in orbit : a pictorial & verbal history of the International Space Station

 https://welib.org/md5/afdda3b38bd154539b8b02b22ad0de17

February 28,2004

 https://en.wikipedia.org/wiki/Periodic_table

November 17,2019

 https://planet4589.org/space/jsr/back/news.771.txt

I was a teenage space reporter : from Apollo 11 to our future in space

 https://welib.org/md5/b0e9366bd4273bef1130d931f187a942

Orion EFT-1

 2014-076A

---

Exploration Flight Test of Orion on Delta 4, two orbits. SV is assembled at Michoud, outfitted at LM/OCF-KSC and then tested at LM/Denver. The flight is operated by LM Space Systems/Denver, rather than by NASA.

Flight capsule, dummy SM and test fairings. SM fairings provide structural strength during stage 1 burn and are jettisoned during the stage 2 burn to save mass.

Mass is 21000 kg including SM and LAS; 8600 kg CM at landing. CM+LAS at lanch 17000 kg. LAS motor is 3464 kg, with 1780 kN thrust. LAS ACS motor is 760 kg. LAS jettison motor is 410 kg, giving a lower limit of 4650 kg to LAS and upper limit of 12350 kg to the CM; infer service module is about 2650 kg. Orion to stage adapter connects to DCSS. Fairings 450 kg x 3.

CM	9400?
SM	2650?
LAS	7650?
Panels	1383
Total	21083
OSA	510

EFT1
Date	Time	Event	Orbit
2014 Dec 5	1205	Launch by Delta 4H	CC SLC37
		T+3:58 Side CBC MECO, sep
		T+5:31 CBC Core MECO
	1210	T+5:38 Stage 1 sep
	1210	T+5:51 Stage 2 MES
	1211	T+6:16 SM fairings sep
	1211	T+6:20 LAS sep
	1222	T+17:17 Stage 2 MECO-1	185 x 888 x 28.8
	1400	T+1:55:20 Rev 2 Stage 2 MES-2 4:45
		T+2:00:11 MECO-2	-37 x 5807 km x 28.8
	1510	T+3:05 Apogee 5807 km
	1528	T+3:23:36 Stage 2 sep from CM -8.36 113.67 5275 km
	1550	Stage 2 burn 3, 1 min
	1602	T+3:57:11 RCS burn 10s, translation
	1616	T+4:11:05 Stage 2 reentry over Pacific
	1618	T+4:13:35 Orion reentry interface 8.9 km/s
		T+4:19:29 Forward bay cover sep, para deploy
	1629	T+4:23:29 Splashdown off Baja
		23.60N 116.46W
		Recovery by USS Anchorage

Iron, fire, and ice : the real history that inspired Game of Thrones

 https://welib.org/md5/1f28f5f17603b4c579c97849229f6b83

Emotions in Medieval Arthurian Literature: Body, Mind, Voice

 https://welib.org/md5/399d4375cd34cfd29d3fe8707dd71ad9

October 19,2019

 https://planet4589.org/space/jsr/back/news.770.txt

Paperback crush : the totally radical history of '80s and '90s teen fiction

 https://welib.org/md5/0d797d2762397436646aba5a2a5a7273