Progress M-SO1

 2001-041A

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Progress M-SO1 is a modified vehicle, serial 301 (essentially the Progress service module) used to deliver the 240GK Pirs module to the ISS.

M-SO1
Date	Time	Event	Orbit
2001 Sep 14	2334:55	Launch by Soyuz-U No 677
		T+1:58 Blok BVGD sep
		T+2:37 GO sep
		T+4:47 St 2 sep
		T+5:01 KhO sep
		T+8:45 Blok I MECO
	2343:44	T+8:49 Blok-I sep	88.0? 170 x 180 x 51.6
2001 Sep 15	0320:57	DV1A 47s 18.4m/s
	0358:02	DV1B 9.6m/s 25s
2001 Sep 16	0029:47	DV2 6.3s 2.0m/s
	1153		89.55 239 x 265 x 51.6
2001 Sep 16	2230	Begin auto docking sequence
	2255	DV3A Burn 26m/s
	2301		89.53 238 x 264 x 51.6
	2318	DV3B Burn 1m/s
	2341	MC1 Burn 43 m/s
2001 Sep 17	0026	MC2 Burn 7m/s
	0032	MC3 Burn 5m/s
	0034	MC4 Burn 1.5m/s
	0038	At 200m, begin flyaround
	0045	At 165m, stationkeep below Zvezda
	0105:14	Docked with Zvezda nadir
			92.36 385 x 395 x 51.6
		HO to ISS
2001 Sep 26	1536	Progress undocks
	1545	Progress sep burn
	1600	Progress at range 24 km
	2330	Progress deorbit 609.8s 102.3m/s
2001 Sep 27	0009	Reentry over Pacific

FIRE 1

  1964-U02

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The Project FIRE High Velocity Reentry Package studied a blunt body reentry at 11.3 km/s and 15 degree angle. Total launch mass was 2000 kg including the velocity package shell and control system, 1400 kg without but including the Antares IIA5 with 1179 kg of propellant. Fairing is a modified DAC Nimbus fairing. Velocity package contractor was LTV. Reentry package was Republic Aviation Corp. Planned apogee was 837 km.

FIRE 1 reached 11.5736 km/s (or 11.52 km/s, TN-D-2996) at 16.6W 7.8S, 122 km on descent from 840 km, at an angle of -14.608 deg and azimuth 122.5 deg. Range was 8370 km. Possible initial trajectory -2900 x 840 x 30.0. Post burn trajectory -219 x Inf x 32 deg.

FIRE 1
Date	Time	Event	Orbit
1964 Apr 14	2142:25	Launch by Atlas 263D	CKAFS LC12
	2144:38	T+2:13 BECO, 24.4 deg ascent
	2144:39?	Booster sep
	2147:13	T+4:48 SECO
	2147:20	VP fairing jettison
	2147:31	T+5:09 VECO, 8.0 deg ascent
	2147:25	6.28km/s rel, 15.0 deg 299 km	-2920 x 840 x 31.1
	2147:36	Spacecraft sep from Atlas
	2147:45	Fire 1 orientation
	2149:26	Coast phase
	2158:05	Apogee 840 km
	2208:39	Spinup
	2208:42	Velocity package shell sep
		299.43 km -15.32 deg 6.3395 km/s rel	-2820 x 841 x 30.8?
	2208:45	Antares burn dV = 5.2km/s
	2209:17	Antares burnout
	2209:43	Simulation fidiucial time 149.5 km -15 deg 11.55 km/s
	2209:45	Reentry package sep	-219 x -51626 x 32.1
	2209:52	Reentry 122 km 11.5736 km/s -14.608 deg 16.7W 7.8S
	2209:57	Yaw disturbance; Antares bow shock hits Fire
	2210:14	Heat shield 1 sep
	2210:21	Heat shield 2 sep
	2210:31	End of blackout
	2215:10	Impact 10.227S 12.643W

Aviation Week: July 2,2001

 https://welib.org/md5/234ea3df7bf1473269d9c6d622535968