Ground Ignition Weights

 

Weights In Pounds Mass

Apollo 7

Apollo 8

Apollo 9

Apollo 10

Apollo 11

Apollo 12

Apollo 13

Apollo 14

Apollo 15

Apollo 16

Apollo 17

 

 

 

 

 

 

 

 

 

 

 

 

Ground Ignition Time

Relative to Range Zero (sec)

 

-2.988

 

-6.585

 

-6.3

 

-6.4

 

-6.4

 

-6.5

 

-6.7

 

-6.5

 

-6.5

 

-6.7

 

-6.9

 

 

 

 

 

 

 

 

 

 

 

 

S-IB stage, dry

84,530

---

---

---

---

---

---

---

---

---

---

S-IB stage, oxidizer

631,300

---

---

---

---

---

---

---

---

---

---

S-IB stage, fuel

276,900

---

---

---

---

---

---

---

---

---

---

S-IB stage, other

1,182

---

---

---

---

---

---

---

---

---

---

S-IB stage, total

993,912

---

---

---

---

---

---

---

---

---

---

 

 

 

 

 

 

 

 

 

 

 

 

S-IB/S-IVB interstage, dry

5,543

---

---

---

---

---

---

---

---

---

---

Retromotor Propellant

1,061

---

---

---

---

---

---

---

---

---

---

 

 

 

 

 

 

 

 

 

 

 

 

S-IC stage, dry

---

305,232

294,468

293,974

287,531

287,898

287,899

287,310

286,208

287,855

287,356

S-IC stage, oxidizer

---

3,128,034

3,301,203

3,302,827

3,305,786

3,310,199

3,304,734

3,312,769

3,312,030

3,311,226

3,314,388

S-IC stage, fuel

---

1,357,634

1,431,678

1,423,254

1,424,889

1,424,287

1,431,384

1,428,561

1,410,798

1,439,894

1,431,921

S-IC stage, other

---

6,226

5,508

5,491

5,442

5,442

5,401

5,194

4,283

5,396

5,395

S-IC stage, total

---

4,797,126

5,032,857

5,025,546

5,023,648

5,027,826

5,029,418

5,033,834

5,013,319

5,044,371

5,039,060

 

 

 

 

 

 

 

 

 

 

 

 

S-IC/S-II interstage, dry

---

12,436

11,591

11,585

11,477

11,509

11,454

11,400

9,083

10,091

9,975

 

 

 

 

 

 

 

 

 

 

 

 

S-II stage, dry

---

88,500

84,312

84,273

79,714

80,236

77,947

78,120

78,908

80,362

80,423

S-II stage, oxidizer

---

793,795

821,504

823,325

819,050

825,406

836,741

837,484

837,991

846,157

844,094

S-II stage, fuel

---

154,907

158,663

158,541

158,116

157,986

159,931

159,232

158,966

160,551

160,451

S-II stage, other

---

1,426

1,188

1,250

1,260

1,250

1,114

1,051

1,082

991

934

S-II stage, total

---

1,038,628

1,065,667

1,067,389

1,058,140

1,064,878

1,075,733

1,075,887

1,076,947

1,088,061

1,085,902

 

 

 

 

 

 

 

 

 

 

 

 

S-II/S-IVB interstage, dry

---

8,731

7,998

8,045

8,076

8,021

8,081

8,060

8,029

8,055

8,019

 

 

 

 

 

 

 

 

 

 

 

 

S-IVB stage, dry

21,852

25,926

25,089

25,680

24,852

25,064

25,097

25,030

25,198

25,099

25,040

S-IVB stage, oxidizer

193,330

192,840

189,686

192,089

192,497

190,587

191,890

190,473

195,788

195,372

195,636

S-IVB stage, fuel

39,909

43,395

43,709

43,388

43,608

43,663

43,657

43,546

43,674

43,727

43,752

S-IVB stage, other

1,432

1,626

1,667

1,684

1,656

1,873

1,673

1,687

1,655

1,643

1,658

S-IVB stage, total

256,523

263,787

260,151

262,841

262,613

261,187

262,317

260,736

266,315

265,841

266,086

 

 

 

 

 

 

 

 

 

 

 

 

Total Instrument Unit

4,263

4,842

4,281

4,267

4,275

4,277

4,502

4,505

4,487

4,502

4,470

 

 

 

 

 

 

 

 

 

 

 

 

Spacecraft/Lunar Module Adapter

3,943

3,951

4,012

3,969

3,951

3,960

3,947

3,962

3,964

3,961

3,961

LM (LTA Apollo 8)

---

19,900

32,034

30,735

33,278

33,562

33,493

33,685

36,238

36,237

36,262

Command and Service Module

32,495

63,531

59,116

63,560

63,507

63,559

63,795

64,448

66,925

66,949

66,942

Total Launch Escape System

8,874

8,890

8,869

8,936

8,910

8,963

8,991

9,027

9,108

9,167

9,104

Total Spacecraft (CSM)

45,312

96,272

104,031

107,200

109,646

110,044

110,226

111,122

116,235

116,314

116,269

 

 

 

 

 

 

 

 

 

 

 

 

Total Vehicle

1,306,614

6,221,823

6,486,577

6,486,873

6,477,875

6,487,742

6,501,733

6,505,548

6,494,415

6,537,238

6,529,784

Actual weights at S-IC stage ignition, compiled from Saturn launch vehicle flight evaluation reports. Weights to do not add to vehicle totals due to truncated decimal data in report.

 

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